This disclosure is directed toward power machines. More particularly, the present disclosure is directed to power machines that operate in whole or in part under electrical power. Power machines, for the purposes of this disclosure, include any type of machine that generates power for the purpose of accomplishing a particular task or a variety of tasks. One type of power machine is a work vehicle. Work vehicles, such as loaders, are generally self-propelled vehicles that have a work device, such as a lift arm (although some work vehicles can have other work devices) that can be manipulated to perform a work function. Work vehicles include loaders, excavators, utility vehicles, tractors, and trenchers, to name a few examples.
The discussion above is merely provided for general background information and is not intended to be used as an aid in determining the scope of the claimed subject matter.
Some configurations of the disclosure are directed to implementing force balancing for power machines and, in particular, to providing force balancing such that a pair of electric actuators of electric power machines exert substantially balanced forces when acting on a common load. Configurations described herein can thus facilitate automated force balancing for electric power machines. Accordingly, the technology disclosed herein may provide an advantageous control scheme that enables electric actuator force balancing on an electric power machine with paired electric actuators.
In some examples, force balancing may be implemented by matching electric currents for the electric actuators. For instance, in some examples, a first electric actuator may be controlled via a velocity control scheme and a second electric actuator may be controlled via an electric current control scheme, where the electric current of the second electric actuator may be controlled based on an electric current of the first electric actuator. In other examples, electric currents of the paired electric actuators may be monitored for electric current differences between the actuators. In such examples, when an electric current difference is detected, one or more of the electric actuators may be controlled via a velocity control scheme, where electric current differences may be compensated for via velocity adjustments (e.g., increasing or decreasing velocity for one or more of the electric actuators based on the mismatched currents). In still other examples, the paired electric actuators may be controlled via an electric control scheme, where a commanded movement can be implemented by using the same electric current to control each of the paired electric actuators.
Some configurations of the present disclosure provide an electric power machine. The electric power machine may include a power machine frame. The electric power machine may include a plurality of electric actuators supported by the power machine frame, where the plurality of electric actuators may include a set of electric lift actuators and a set of electric tilt actuators. The electric power machine may include a lift arm structure that may include: a lift arm coupled to the power machine frame and configured to be moved relative to the power machine frame by the set of electric lift actuators; and a work element supported by the lift arm and configured to be moved relative to the lift arm by the set of electric tilt actuators. The electric power machine may include an electrical power source configured to power the plurality of electric actuators. The electric power machine may include one or more electronic processors in communication with the plurality of electric actuators. The one or more electronic processors may be configured to: receive a command for movement of the lift arm using the set of electric lift actuators or movement of the work element using the set of electric tilt actuators; and control, based on the command, the set of electric lift actuators or the set of electric tilt actuators to, respectively, substantially balance forces between the set of electric lift actuators or substantially balance forces between the set of electric tilt actuators.
Some configurations described herein provide a method for controlling an electric power machine. The method may include receiving, with one or more electronic processors, a command to perform an operation with a plurality of electric actuators of the electric power machine, the plurality of electric actuators including a first electric actuator and a second electric actuator. The method may include controlling, with the one or more electronic processors, the first electric actuator based on a velocity control parameter to perform the operation. The method may include determining, with the one or more electronic processors, a target electric current for the second electric actuator based on a present electric current of the first electric actuator while the first electric actuator is controlled based on the velocity control parameter to perform the operation. The method may include controlling, with the one or more electronic processors, the second electric actuator based on the target electric current to perform the operation.
Some configurations described herein provide a method for controlling an electric power machine. The method may include receiving, with one or more electronic processors, a command for controlling a work element with a plurality of electric actuators of the electric power machine. The method may include determining, with the one or more electronic processors, a target velocity for the plurality of electric actuators based on the command. The method may include controlling, with the one or more electronic processors, the plurality of electric actuators based on the target velocity. The method may include, while controlling the plurality of electric actuators based on the target velocity, monitoring, with the one or more electronic processors, electric currents of a first electric actuator and a second electric actuator of the plurality of electric actuators to detect an electric current difference between the electric currents of the first electric actuator and the second electric actuator. The method may include, responsive to detecting the electric current difference: determining, with the one or more electronic processors, a first adjusted target velocity for the first electric actuator; and controlling, with the one or more electronic processors, the first electric actuator based on the first adjusted target velocity.
This Summary and the Abstract are provided to introduce a selection of concepts in a simplified form that are further described below in the Detailed Description. The Summary and the Abstract are not intended to identify key features or essential features of the claimed subject matter, nor are they intended to be used as an aid in determining the scope of the claimed subject matter.
The following drawings are provided to help illustrate various features of examples of the disclosure and are not intended to limit the scope of the disclosure or exclude alternative implementations.
The concepts disclosed in this discussion are described and illustrated with reference to exemplary embodiments. These concepts, however, are not limited in their application to the details of construction and the arrangement of components in the illustrative embodiments and are capable of being practiced or being carried out in various other ways. The terminology in this document is used for the purpose of description and should not be regarded as limiting. Words such as “including,” “comprising,” and “having” and variations thereof as used herein are meant to encompass the items listed thereafter, equivalents thereof, as well as additional items.
While the power machines disclosed herein may be embodied in many different forms, several specific embodiments are discussed herein with the understanding that the embodiments described in the present disclosure are to be considered only exemplifications of the principles described herein, and the technology disclosed herein is not intended to be limited to the embodiments illustrated.
Some discussion below describes improved components and configurations for power machines, including components and configurations that use electrical (e.g., as opposed to hydraulic) power to operate certain power machine components or otherwise implement certain power machine functionality. In some configurations, electrically powered components can be mounted to a frame of a power machine to selectively move work elements of the power machine, including lift arms or implement carriers. In some configurations, electrically powered components can provide motive power for a power machine, including for tracked power machines (e.g., compact tracked loaders).
The technology disclosed herein relates to electric power machines, including automated operation of electric power machines. In particular, the technology disclosed herein relates to systems and methods of controlling sets of electric actuators of a power machine to provide improved force balancing. For example, implementations of the disclosed technology can be used to implement a force balancing control scheme or method that substantially balances forces between electric actuators that act on a common load. This can be particularly useful, for example, to mitigate premature wear (e.g., reduce maintenance, repairs, and downtime) experienced by one or more electric actuators of the paired electric actuators, as may tend to result from imbalanced forces on actuators under conventional control systems. Additionally, some configurations disclosed herein may also reduce (e.g., eliminate) underperformance conditions of the power machine, such as those underperformance conditions resulting from imbalanced forces between the paired electric actuators. As further detailed below, various control methods and system configurations can be used to facilitate automated force balancing for various types of work elements, including for electric actuators of electric power machines in particular.
Accordingly, some configurations of the disclosure are directed to implementing force balancing for power machines and, in particular, to provide force balancing such that a pair of electric actuators of electric power machines exert substantially balanced forces when acting on a common load. Configurations described herein facilitate automated force balancing for electric power machines. Accordingly, the technology disclosed herein may provide an advantageous control scheme that enables electric actuator force balancing on an electric power machine with paired electric actuators.
More specifically, power machines, such as skid-steers, compact track loaders, etc., may utilized sets of actuators that cooperatively provide force to perform a particular task, including lift operations. For example, pairs of actuators may be generally positioned opposite each other on a lift arm assembly, a work element, or other structure. The pairs of actuators may then cooperatively work together to synchronously perform an operation (e.g., a work task), such that each actuator synchronously acts on a common load. For example, the actuators may include a pair of lift actuators that cooperatively perform a lift operation by synchronously exerting a force on a lift arm assembly. As another example, the actuators may include a pair of tilt actuators that cooperatively perform a tilt operation by synchronously adjusting a tilt angle of a work element (e.g., a bucket or other implement).
As such, it may be useful to control sets of actuators for synchronized operation such that the actuators exert balanced forces on a common load (e.g., each actuator provides the same or substantially the same force on the common load). In some cases, hydraulic actuator systems can implement a position control scheme such that each actuator is controlled based on the same velocity (e.g., a commanded or controlled velocity). In hydraulic actuator systems, such a velocity control scheme may inherently maintain balanced forces between cooperating hydraulic actuators (e.g., sets of lift or tilt cylinders) because of the naturally self-correcting action of the hydraulic system.
In contrast, electric actuators are conventionally controlled based on position. However, when electric actuators are controlled to cooperatively perform an operation with respect to a common load, implementing a position control scheme may tend not to result in balanced forces between the actuators (as would be achieved by implementing that position control scheme with a hydraulic actuator system). This is because the precise position control of conventional motor controllers can conflict with the mechanical play and stacked tolerances of the structures of the power machine, with a result that a majority of force loading may tend to fall on only one actuator of a set (e.g., a lift actuator on only one side of a lift arm). In other words, implementing conventional position control for an electric actuator system may not facilitate force balancing between paired electric actuators because the common reference frame assumed by a conventional motor controller may not actually correspond to the real-world positioning and movement of the actuators on a power machine.
Accordingly, implementing a position control scheme in an electric actuator system generally results in unbalanced forces between paired electric actuators. In particular, when a position control scheme is utilized to control a pair of electric actuators, the electric actuators do not exert an equal force on the common load. Rather, one of the electric actuators generally exerts a majority of the force on the common load while the other electric actuator exerts little or no force on the common load. In some examples, the other electric actuator may thus even be pulled along a range of motion by the electric actuator that exerts the majority of the force on the common load, thus further accentuating the imbalanced loading between the actuators.
Such a force imbalance between the paired electric actuators may adversely impact the power machine. For example, the electric actuator that exerts the majority of the force, and that, ultimately, drags the other electric actuator, may experience premature wearing, which may ultimately result in increased maintenance, repairs, and downtime. As another example, the performance of the power machine may be hindered by the force imbalance, such that the power machine underperforms. Accordingly, when actuators cooperatively act on a common load, it can be advantageous to implement particular control schemes so that the forces exerted by the actuators to be substantially balanced.
In some examples, force balancing may be implemented by commanding matching electric currents for sets of electric actuators. For example, a first electric actuator may be controlled via a velocity control scheme and a second electric actuator may be controlled via an electric current control scheme, where the electric current of the second electric actuator may be controlled based on an electric current provided to the first electric actuator under the velocity control scheme. In other examples, electric currents of the set of electric actuators may be monitored for electric current differences. In such examples, when an electric current difference is detected, one or more of the electric actuators may be controlled via a velocity control scheme, where automatic velocity adjustments at one or more of the electric actuators (e.g., increasing or decreasing velocity for one or more of the electric actuators) can compensate for electric current differences between the actuators. In still other examples, the set of electric actuators may be controlled via an electric current control scheme, where the same commanded electric current may be used to affect control for each of the set of electric actuators.
These concepts can be practiced on various power machines, as will be described below. A representative power machine on which the embodiments can be practiced is illustrated in diagram form in
Certain work vehicles have work elements that can perform a dedicated task. For example, some work vehicles have a lift arm to which an implement such as a bucket is attached such as by a pinning arrangement. The work element, i.e., the lift arm can be manipulated to position the implement to perform the task. The implement, in some instances can be positioned relative to the work element, such as by rotating a bucket relative to a lift arm, to further position the implement. Under normal operation of such a work vehicle, the bucket is intended to be attached and under use. Such work vehicles may be able to accept other implements by disassembling the implement/work element combination and reassembling another implement in place of the original bucket. Other work vehicles, however, are intended to be used with a wide variety of implements and have an implement interface such as implement interface 170 shown in
On some power machines, implement interface 170 can include an implement carrier, which is a physical structure movably attached to a work element. The implement carrier has engagement features and locking features to accept and secure any of a number of different implements to the work element. One characteristic of such an implement carrier is that once an implement is attached to it, it is fixed to the implement (i.e., not movable with respect to the implement) and when the implement carrier is moved with respect to the work element, the implement moves with the implement carrier. The term implement carrier as used herein is not merely a pivotal connection point, but rather a dedicated device specifically intended to accept and be secured to various different implements. The implement carrier itself is mountable to a work element 130 such as a lift arm or the frame 110. Implement interface 170 can also include one or more power sources for providing power to one or more work elements on an implement. Some power machines can have a plurality of work element with implement interfaces, each of which may, but need not, have an implement carrier for receiving implements. Some other power machines can have a work element with a plurality of implement interfaces so that a single work element can accept a plurality of implements synchronously. Each of these implement interfaces can, but need not, have an implement carrier.
Frame 110 includes a physical structure that can support various other components that are attached thereto or positioned thereon. The frame 110 can include any number of individual components. Some power machines have frames that are rigid. That is, no part of the frame is movable with respect to another part of the frame. Other power machines have at least one portion that can move with respect to another portion of the frame. For example, excavators can have an upper frame portion that rotates with respect to a lower frame portion. Other work vehicles have articulated frames such that one portion of the frame pivots with respect to another portion for accomplishing steering functions.
Frame 110 supports the power source 120, which is configured to provide power to one or more work elements 130 including the one or more tractive elements 140, as well as, in some instances, providing power for use by an attached implement via implement interface 170. Power from the power source 120 can be provided directly to any of the work elements 130, tractive elements 140, and implement interfaces 170. Alternatively, power from the power source 120 can be provided to a control system 160, which in turn selectively provides power to the elements that capable of using it to perform a work function. Power sources for power machines typically include an engine such as an internal combustion engine and a power conversion system such as a mechanical transmission or a hydraulic system that is configured to convert the output from an engine into a form of power that is usable by a work element. Other types of power sources can be incorporated into power machines, including electric sources or a combination of power sources, known generally as hybrid power sources.
Power machine 100 includes an operator station 150 that includes an operating position from which an operator can control operation of the power machine. In some power machines, the operator station 150 is defined by an enclosed or partially enclosed cab. Some power machines on which the disclosed embodiments may be practiced may not have a cab or an operator compartment of the type described above. For example, a walk behind loader may not have a cab or an operator compartment, but rather an operating position that serves as an operator station from which the power machine is properly operated. More broadly, power machines other than work vehicles may have operator stations that are not necessarily similar to the operating positions and operator compartments referenced above. Further, some power machines such as power machine 100 and others, whether or not they have operator compartments or operator positions, may be capable of being operated remotely (i.e., from a remotely located operator station) instead of or in addition to an operator station adjacent or on the power machine. This can include applications where at least some of the operator-controlled functions of the power machine can be operated from an operating position associated with an implement that is coupled to the power machine. Alternatively, with some power machines, a remote-control device can be provided (i.e., remote from both of the power machine and any implement to which is it coupled) that is capable of controlling at least some of the operator-controlled functions on the power machine.
Loader 200 is one particular example of the power machine 100 illustrated broadly in
Loader 200 includes frame 210 that supports a power system 220, the power system being capable of generating or otherwise providing power for operating various functions on the power machine. Power system 220 is shown in block diagram form but is located within the frame 210. Frame 210 also supports a work element in the form of a lift arm assembly 230 that is powered by the power system 220 and that can perform various work tasks. As loader 200 is a work vehicle, frame 210 also supports a traction system 240, which is also powered by power system 220 and can propel the power machine over a support surface. The lift arm assembly 230 in turn supports an implement interface 270, which includes an implement carrier 272 that can receive and secure various implements to the loader 200 for performing various work tasks and power couplers 274, to which an implement can be coupled for selectively providing power to an implement that might be connected to the loader. Power couplers 274 can provide sources of hydraulic or electric power or both. The loader 200 includes a cab 250 that defines an operator station 255 from which an operator can manipulate various control devices 260 to cause the power machine to perform various work functions. Cab 250 can be pivoted back about an axis that extends through mounts 254 to provide access to power system components as needed for maintenance and repair.
The operator station 255 includes an operator seat 258 and a plurality of operation input devices, including control levers 260 that an operator can manipulate to control various machine functions. Operator input devices can include buttons, switches, levers, sliders, pedals and the like that can be stand-alone devices such as hand operated levers or foot pedals or incorporated into hand grips or display panels, including programmable input devices. Actuation of operator input devices can generate signals in the form of electric signals, hydraulic signals, and/or mechanical signals. Signals generated in response to operator input devices are provided to various components on the power machine for controlling various functions on the power machine. Among the functions that are controlled via operator input devices on power machine 200 include control of the tractive elements 219, the lift arm assembly 230, the implement carrier 272, and providing signals to any implement that may be operably coupled to the implement.
Loaders can include human-machine interfaces including display devices that are provided in the cab 250 to give indications of information relatable to the operation of the power machines in a form that can be sensed by an operator, such as, for example audible and/or visual indications. Audible indications can be made in the form of buzzers, bells, and the like or via verbal communication. Visual indications can be made in the form of graphs, lights, icons, gauges, alphanumeric characters, and the like. Displays can provide dedicated indications, such as warning lights or gauges, or dynamic to provide programmable information, including programmable display devices such as monitors of various sizes and capabilities. Display devices can provide diagnostic information, troubleshooting information, instructional information, and various other types of information that assists an operator with operation of the power machine or an implement coupled to the power machine. Other information that may be useful for an operator can also be provided. Other power machines, such walk behind loaders may not have a cab nor an operator compartment, nor a seat. The operator position on such loaders is generally defined relative to a position where an operator is best suited to manipulate operator input devices.
Various power machines that can include and/or interacting with the embodiments discussed herein can have various different frame components that support various work elements. The elements of frame 210 discussed herein are provided for illustrative purposes and frame 210 is not the only type of frame that a power machine on which the embodiments can be practiced can employ. Frame 210 of loader 200 includes an undercarriage or lower portion 211 of the frame and a mainframe or upper portion 212 of the frame that is supported by the undercarriage. The mainframe 212 of loader 200, in some embodiments is attached to the undercarriage 211 such as with fasteners or by welding the undercarriage to the mainframe. Alternatively, the mainframe and undercarriage can be integrally formed. Mainframe 212 includes a pair of upright portions 214A and 214B located on either side and toward the rear of the mainframe that support lift arm assembly 230 and to which the lift arm assembly 230 is pivotally attached. The lift arm assembly 230 is illustratively pinned to each of the upright portions 214A and 214B. The combination of mounting features on the upright portions 214A and 214B and the lift arm assembly 230 and mounting hardware (including pins used to pin the lift arm assembly to the mainframe 212) are collectively referred to as joints 216A and 216B (one is located on each of the upright portions 214) for the purposes of this discussion. Joints 216A and 216B are aligned along an axis 218 so that the lift arm assembly is capable of pivoting, as discussed below, with respect to the frame 210 about axis 218. Other power machines may not include upright portions on either side of the frame or may not have a lift arm assembly that is mountable to upright portions on either side and toward the rear of the frame. For example, some power machines may have a single arm, mounted to a single side of the power machine or to a front or rear end of the power machine. Other machines can have a plurality of work elements, including a plurality of lift arms, each of which is mounted to the machine in its own configuration. Frame 210 also supports a pair of tractive elements in the form of wheels 219A-D on either side of the loader 200.
The lift arm assembly 230 shown in
The lift arm assembly 230 has a pair of lift arms 234 that are disposed on opposing sides of the frame 210. A first end 232A of each of the lift arms 234 is pivotally coupled to the power machine at joints 216 and a second end 232B of each of the lift arms is positioned forward of the frame 210 when in a lowered position as shown in
Each of the lift arms 234 has a first portion 234A of each lift arm 234 is pivotally coupled to the frame 210 at one of the joints 216 and the second portion 234B extends from its connection to the first portion 234A to the second end 232B of the lift arm assembly 230. The lift arms 234 are each coupled to a cross member 236 that is attached to the first portions 234A. Cross member 236 provides increased structural stability to the lift arm assembly 230. A pair of actuators 238, which on loader 200 are hydraulic cylinders configured to receive pressurized fluid from power system 220, are pivotally coupled to both the frame 210 and the lift arms 234 at pivotable joints 238A and 238B, respectively, on either side of the loader 200. The actuators 238 are sometimes referred to individually and collectively as lift cylinders. Actuation (i.e., extension and retraction) of the actuators 238 cause the lift arm assembly 230 to pivot about joints 216 and thereby be raised and lowered along a fixed path illustrated by arrow 237. Each of a pair of control links 217 are pivotally mounted to the frame 210 and one of the lift arms 232 on either side of the frame 210. The control links 217 help to define the fixed lift path of the lift arm assembly 230.
Some lift arms, most notably lift arms on excavators but also possible on loaders, may have portions that are controllable to pivot with respect to another segment instead of moving in concert (i.e., along a pre-determined path) as is the case in the lift arm assembly 230 shown in
An implement interface 270 is provided proximal to a second end 232B of the lift arm assembly 230. The implement interface 270 includes an implement carrier 272 that is capable of accepting and securing a variety of different implements to the lift arm 234. Such implements have a complementary machine interface that is configured to be engaged with the implement carrier 272. The implement carrier 272 is pivotally mounted at the second end 232B of the arm 234. Implement carrier actuators 235 are operably coupled the lift arm assembly 230 and the implement carrier 272 and are operable to rotate the implement carrier with respect to the lift arm assembly. Implement carrier actuators 235 are illustratively hydraulic cylinders and often known as tilt cylinders.
By having an implement carrier capable of being attached to a plurality of different implements, changing from one implement to another can be accomplished with relative ease. For example, machines with implement carriers can provide an actuator between the implement carrier and the lift arm assembly, so that removing or attaching an implement does not involve removing or attaching an actuator from the implement or removing or attaching the implement from the lift arm assembly. The implement carrier 272 provides a mounting structure for easily attaching an implement to the lift arm (or other portion of a power machine) that a lift arm assembly without an implement carrier does not have.
Some power machines can have implements or implement like devices attached to it such as by being pinned to a lift arm with a tilt actuator also coupled directly to the implement or implement type structure. A common example of such an implement that is rotatably pinned to a lift arm is a bucket, with one or more tilt cylinders being attached to a bracket that is fixed directly onto the bucket such as by welding or with fasteners. Such a power machine does not have an implement carrier, but rather has a direct connection between a lift arm and an implement.
The implement interface 270 also includes power coupler(s) 274 available for connection to an implement on the lift arm assembly 230. The power coupler(s) 274 includes pressurized hydraulic fluid port to which an implement can be removably coupled. The pressurized hydraulic fluid port selectively provides pressurized hydraulic fluid for powering one or more functions or actuators on an implement. The power coupler can also include an electric power source for powering electric actuators and/or an electronic controller on an implement. The power coupler(s) 274 also exemplarily includes electric conduits that are in communication with a data bus on the excavator 200 to allow communication between a controller on an implement and electronic devices on the loader 200.
Frame 210 supports and generally encloses the power system 220 so that the various components of the power system 220 are not visible in
The description of power machine 100 and loader 200 above is provided for illustrative purposes, to provide illustrative environments on which the embodiments discussed below can be practiced. While the embodiments discussed can be practiced on a power machine such as is generally described by the power machine 100 shown in the block diagram of
In the illustrated example, the power machine 400 can be an electrically powered power machine and thus the power source 402 can include an electric power source such as, for example, a battery pack that includes one or more battery cells (e.g., lithium-ion batteries). In some embodiments, the power source 402 can include other electric storage devices (e.g., a capacitor), and other power sources. In addition, the power machine 400 can, but need not, include an internal combustion engine that provides, via a generator, electric power to the power source 402 (e.g., to charge one or more batteries of the electric power source).
Generally, the control device 404 can be implemented in a variety of different ways and can include one or more types or instances of known electronic controllers. For example, the control device 404 can be implemented as known types of processor devices, (e.g., microcontrollers, field-programmable gate arrays, programmable logic controllers, logic gates, etc.), including as part of one or more general or special purpose computers. In addition, the control device 404 can also include or be in operative communication with other computing components, including memory, inputs, output devices, etc. (not shown). In this regard, the control device 404 can be configured to implement some or all of the operations of the processes described herein, which can, as appropriate, be retrieved from or otherwise interact with memory. In some embodiments, the control device 404 can include multiple control devices (or modules) that can be integrated into a single component or arranged as multiple separate components. In some embodiments, the control device 404 can be part of a larger control system (e.g., the control system 160 of
In different embodiments, different types of actuators can be configured to operate under power from the power source 402, including electric actuators configured as rotary actuators, linear actuators, and combinations thereof. In the example shown in
Also as shown in the example of
Thus, generally, each motor 416, 420 can be controlled to implement particular functionality for the power machine 400. As generally noted above, different configurations of multiple drive or workgroup actuators can be included in some cases (e.g., multiple instances of the actuators 406, 408 as shown), to provide different functionality for a particular power machine. For example, in some configurations, the power machine 400 can include an electric actuator that is a first lift actuator on a first lateral side of the power machine 400, an electric actuator that is a second lift actuator on a second lateral side of the power machine 400, an electric actuator that is a first tilt actuator that is on a first lateral side of the implement interface of the power machine 400, an electric actuator that is a second tilt actuator that is on a second lateral side of the implement interface of the power machine 400, an electric actuator that is a first drive actuator for a first drive system that is on (or otherwise powers one or more tractive elements for) the first lateral side of the power machine 400, and an electric actuator that is a second drive actuator for a second drive system that is on (or otherwise powers one or more tractive elements for) the second lateral side of the power machine 400.
As also noted above, the brakes 410, 412 can be coupled to (e.g., included in) the respective electric actuators 406, 408 in some embodiments. In this regard, a wide variety of known brake systems can be used. For example, one or more brakes can be a mechanical brake that includes a mechanical stop that can be moved into engagement to block movement of a relevant extender or relevant motor, in one or more directions, and can be moved out of engagement to allow movement of the relevant extender or motor. In some cases, a mechanical brake can include an arm that contacts a lead screw of an extender to block further movement of the lead screw. In some embodiments, one or more electrically powered brakes can be provided (i.e., brake assemblies that include one or more electric actuators for application of braking force).
As shown in
As shown in
In some embodiments, similarly to each of the electric loads of the power machine 400, the electric power source of the power source 402 can include (or can be otherwise electrically connected to) an electric current source (e.g., a power electronics board) that adjusts (e.g., and can restrict) the amount of power to be delivered to the electric loads of the power machine 400. In this case, the control device 404 can adjust the driving signal to the electric power source to adjust the total amount of electric current and thus the amount of power delivered to the electric loads of the power machine 400. For example, the control device 404 can adjust the output from the electric power source 402 to regulate the torque, position, direction, and speed of one or more motors powered by the power source 402.
In some embodiments, the control device 404 can be configured to determine a present (i.e., temporally current) power usage of one or more actuators or other electric loads, or a present power delivery from a power source. In some cases, a present power usage or delivery can be measured instantaneously. In some cases, a present power usage or delivery can be measured as an average power delivery over a recent time interval (e.g., a preceding 2 seconds). Thus, for example, the control device 404 can determine a present power usage for each electric load of the power machine 400, or can determine a present power delivery from the electric power source of the power source 402.
In some cases, each electric load of the power machine 400, and the power source 402 can include or can otherwise be electrically connected to an electric current sensor to determine the electric current being provided to (or by) the particular electric component, and a voltage being provided to (or by) the particular electric component can also be determined (e.g., based on voltage sensor or a fixed voltage provided by the power source 402). In this way, for example, the control device 404 can receive information about a present voltage and a present electric current that is delivered to each individual electric load, or about the present voltage and electric current that is supplied by the electric power source of the power machine 400 in total and can thereby determine a present power usage for relevant (e.g., all) electric loads and for the electric power source of the power machine 400.
In some embodiments, the control device 404 can determine a present power usage for the electric power source of the power machine 400 by adding the present power usage for each relevant electric load of the power machine 400 (e.g., as determined by multiplying electric current and voltage for the loads). Alternatively, for example, power can be determined by multiplying the torque and speed of one or more relevant motors. In certain circumstances, it may be advantageous to use either of these known methods. In other cases, the control device 404 can determine a present power usage of the electric power source of the power machine 400 only by determining the power delivered by the electric power source. For example, the control device 404 can receive a present value for electric current delivered by the electric power source 402 and, based on the voltage of the electric power source 402, can then determine a total present power usage for the electric power source. In some cases, the control device 404 can assume a substantially constant voltage for the electric power source and can then determine the present power usage of the electric power source by using the constant voltage and the present electric current value.
In some embodiments, the electric power source 402 can include or can be electrically connected to a sensor to sense a present remaining energy of the electric power source. In some cases, for example, a voltage sensor can sense the voltage of the electric power source, which can be indicative of the present remaining energy left within the electric power source (e.g., because the voltage of the electric power source can be related to the present remaining energy within the electric power source). Any suitable means for sensing the remaining energy of the electric power source can be used, including an accounting of how much electric current is supplied by the energy storage device over time.
In some embodiments, the power machine 400 can include one or more sensors that can sense various aspects of the power machine 400. For example, the power machine 400 can include a torque sensor for one or more electric actuators, to sense a present torque of the one or more electric actuator. In some cases, the torque sensor can be the same as the electric current sensor electrically connected to the electric actuator (e.g., because electric current is related to the torque). As another example, the power machine 400 can include a position sensor for one or more extenders or other components of one or more electric actuators (as appropriate), including as may sense a present extension amount for an extender of an electric actuator (e.g., relative to the housing of the electric actuator). In some cases, this can be a hall-effect sensor, a rotary encoder for the motor (e.g., which can be used to determine the extension amount of actuators with extenders), an optical sensor, etc. In some cases, as shown in
In some cases, the electric power source 526 can be implemented in a similar manner as the previously described power sources (e.g., the power source 402). Thus, the electric power source 526 can include a battery pack including one or more batteries. In general, the electric power source 526 can supply power to some or all of the electric loads of the power machine 500. For example, the electric power source 526 can provide power to the lift electric actuator 518, the electric tilt actuator 522, the drive system 528, the climate control system 536, etc.
The power machine 500 can also include a control device 546 (e.g., a general or special purpose electronic computer or other electronic controller) that can be in communication with the power source 526 and some (or all) of the electric loads of the power machine 500, as appropriate. For example, the control device 546 can be in communication with the lift electric actuator 518, the electric tilt actuator 522, the drive system 528, the climate control system 536, etc. In this way, the control device 546 can control operation of these components, or related other systems, to adjust how power is routed to each of these electric loads (e.g., depending on the criteria defined by a particular power management mode) and, correspondingly, how these components operate under power from the power source 526.
As illustrated in
In the illustrated example, the workgroup electric actuators 660 of the workgroup system 620 include an electric lift actuator 675 and an electric tilt actuator 680 (e.g., an electric lift actuator and an electric tilt actuator, respectively). Generally, lift and tilt actuators corresponding to the electric lift actuator 675 and the electric tilt actuator 680 are described in greater detail herein with respect to
In some configurations, the workgroup electric actuators 660 may include a pair of workgroup electric actuators 660. A pair of workgroup electric actuators 660 may include two or more workgroup electric actuators 660 (e.g., a first workgroup electric actuator, a second workgroup electric actuator, a third workgroup electric actuator, etc.). For example, the pair of workgroup electric actuators 660 may include a pair of electric tilt actuators 680 (e.g., a first electric tilt actuator, a second electric tilt actuator, a third electric tilt actuator, etc.), a pair of electric lift actuators 675 (e.g., a first electric lift actuator, a second electric lift actuator, a third electric lift actuator, etc.). A pair of workgroup electric actuators 660 may be controlled to cooperatively perform an operation or work task. For example, when the pair of workgroup electric actuators 660 includes a first electric lift actuator and a second electric lift actuator, the first and second electric lift actuators may be controlled to cooperatively perform a lift operation, such as, e.g., increasing or decreasing a position of the lift arm 670. As another example, when the pair of workgroup electric actuators 660 includes a first electric tilt actuator and a second electric tilt actuator, the first and second electric tilt actuators may be controlled to cooperatively perform a tilt operation, such as, e.g., adjusting a tilt angle between the work element 655 and the lift arm 670.
The workgroup position sensors 667 can be configured to measure a linear extension or angular orientation of an actuator or other component of a workgroup, with the work group tilt sensor 669 in particular arranged to measure a degree of tilt between the work element 655 and the lift arm 670 (although other tilt measurements are possible). The workgroup electric current sensors 668 can be configured to measure the electric current being provided to one or more of the workgroup electric actuator(s) 660. In some cases, a torque sensor can be used as the workgroup electric current sensor 668 (e.g., because electric current is related to the torque). In some examples, one or more of the workgroup position sensors 667 or the workgroup electric current sensors 668 can be integrated into one or more of the workgroup electric actuators 660 (e.g., can be included as part of the electric tilt or lift actuators 675, 680).
The workgroup electric current sensor(s) 668 may collect information about a present electric current that is delivered to the workgroup electric actuator(s) 660. The workgroup position sensor(s) 667 may collect position data for the power machine 600 (or a component thereof). As one example, the workgroup position sensor 667 may be associated with one of the workgroup electric actuators 660, and may detect position data for the associated workgroup electric actuator 660. For example, the workgroup position sensors 667 may measure or otherwise indicate rotational position data for an electric servo motor. As another example, the workgroup position sensors 667 may be associated with extenders of the workgroup electric actuators 660 (e.g., ball screws or other motor-driven extenders). Accordingly, in some configurations, the workgroup position sensors 667 may sense a current extension amount (as position data) for the extender of each workgroup electric actuator 660 (e.g., an extension distance relative to a housing of the workgroup electric actuator 660). In some cases, the workgroup position sensor 667 may be a hall-effect sensor, a rotary encoder for the motor (e.g., which can be used to determine the extension amount of actuators with extenders), an optical sensor, etc. Accordingly, in some configurations, position data may include a lift height of the lift arm 670 or the work element 655, an extension amount associated with the electric lift actuator 675, or the like.
As a specific implementation of a position sensor, the workgroup tilt sensor(s) 669 may collect tilt or orientation data for the power machine 600 (or a component thereof). In some configurations, the workgroup tilt sensor 669 may be an angle sensor for each pivotable join of the lift arm 670 of the power machine 600 to determine a current orientation of the lift arm 670 (or the work element(s) 655 coupled thereto). In some configurations, the workgroup tilt sensor 669 may determine a current attitude of a work element 655 relative to the lift arm 670 (e.g., a degree of tilt of an attached bucket or other implement) (as position data).
The power machine 600 may also include the power system 615 (e.g., the power system 120 of
The power machine 600 may also include the control system 610. The control system 610 (e.g., the control system 160 of
In some configurations, the control system 610 receives input from an operator input device, such as one of the operator input devices 262 of
As illustrated in
The communication interface 710 allows the controller 690 to communicate with devices external to the controller 690. For example, as illustrated in
The communication interface 710 may include a port for receiving a wired connection to an external device (for example, a universal serial bus (“USB”) cabled and the like), a transceiver for establishing a wireless connection to an external device (for example, over one or more communication networks, such as the Internet, local area network (“LAN”), a wide area network (“WAN”), and the like), or a combination thereof. In some configurations, the controller 690 can be a dedicated or stand-alone controller. In some configurations, the controller 690 can be part of a system of multiple distinct controllers (e.g., a hub controller, a drive controller, a workgroup controller, etc.) or can be formed by a system of multiple distinct controllers (e.g., also with hub, drive, and workgroup controllers, etc.).
The electronic processor 700 is configured to access and execute computer-readable instructions (“software”) stored in the memory 705. The software may include firmware, one or more applications, program data, filters, rules, one or more program modules, and other executable instructions. For example, the software may include instructions and associated data for performing a set of functions, including the methods described herein.
For example, as illustrated in
A control parameter may be a parameter or value that may affect control of the power machine 600 (or a component thereof). For instance, a control parameter may be implemented as a command issued to a component of the power machine 600 such that, upon receipt of that command, operation of the component of the power machine 600 is controlled using the command. A control parameter may include, e.g., a velocity control parameter, an electric current control parameter, a position control parameter, etc. A velocity control parameter may include, e.g., a commanded or otherwise set velocity (e.g., a target velocity for a control loop) that may be used to affect a velocity of a component of the power machine 600. An electric current control parameter may include, e.g., a commanded or otherwise set electric current (e.g., a target electric current for a control loop) that may be used to affect an electric current of a component of the power machine 600. A position control parameter may include, e.g., a commanded or otherwise set position (e.g., a target position for a control loop) that may be used to affect a position of a component of the power machine 600.
A control scheme may include, e.g., an electric current control scheme, a velocity control scheme, a position control scheme, etc. For instance, when operating pursuant to an electric current control scheme, electric current may be used to control operation of the power machine 600, with control being affected using an electric current control parameter. For example, rather than a target velocity or target position, movement of an electric actuator can be controlled based on a target electric current. When operating in a velocity control scheme, velocity may be used to control operation of the power machine 600, with control being affected using a velocity control parameter. For example, rather than a target electric current or target position, movement of an electric actuator can be controlled based on a target velocity. When operating in a position control scheme, position may be used to control operation of the power machine 600, with control being affected using a position control parameter. For example, rather than a target velocity or target electric current, movement of an electric actuator can be controlled based on a target position.
Accordingly, the application 720 (when executed by the electronic processor 700) may implement a velocity control scheme, an electric current control scheme, or a position control scheme to affect control of the workgroup electric actuator(s) 660 using a velocity control parameter, an electric current control parameter, or a position control parameter, respectively. In some configurations, the application 720 (when executed by the electronic processor 700) may facilitate force balancing for a set of cooperating workgroup electric actuators 660 (e.g., a pair of electric lift actuators or a pair of electric tilt actuators).
As illustrated in
The command may control the lift arm 670, the work element 655, or another component of the power machine 600. In some examples, the command may include a command for controlling the work element 655 with the workgroup electric actuator(s) 660. For example, the command may be a tilt command to perform a tilt operation with the work element 655 by controlling the electric tilt actuator(s) 680 to adjust a tilt angle of the work element 655. In some examples, the command may include a command for controlling the lift arm 670 with the workgroup electric actuator(s) 660. For example, the command may be a lift command to perform a lift operation with the lift arm 670 by controlling the electric lift actuator(s) 675 to raise or lower the lift arm.
In some examples, performance of the operation may involve cooperatively controlling multiple workgroup electric actuators 660, such as, e.g., a set or pair of workgroup electric actuators 660 (e.g., first and second electric tilt actuator, first and second electric lift actuators, or another number of workgroup electric actuators working cooperatively to perform an operation). For example, when the command is a tilt command to adjust a tilt angle between the work element 655 and the lift arm 670, a set of electric tilt actuators 680 (e.g., a first electric tilt actuator and a second electric tilt actuator, or another number of electric tilt actuators working cooperatively to perform the tilt operation) may cooperatively adjust the tilt angle between the work element 655 and the lift arm 670 synchronously. As another example, when the command is a lift command to raise the lift arm 670, a set of electric lift actuators 675 (e.g., a first electric lift actuator and a second electric lift actuator, or another number of electric lift actuators working cooperatively to perform the lift operation) may be controlled such that each electric lift actuator 675 synchronously acts on a common load (e.g., the lift arm 670, the work element 655, etc.) to perform the lift operation.
As illustrated in
As illustrated in
As illustrated in
The electronic processor 700 may control one of the workgroup electric actuators 660 (e.g., the first workgroup electric actuator) based on a velocity control parameter to perform the operation (at block 910). In other words, the electronic processor 700 may implement a velocity control scheme for controlling the first workgroup electric actuator to perform the operation. For example, the electronic processor 700 may determine a target velocity for the first workgroup electric actuator, and may control the first workgroup electric actuator by controlling a velocity of the first workgroup electric actuator based on the target velocity. In some configurations, the electronic processor 700 may determine the velocity control parameter based on the commanded operation (e.g., the command received at block 905). For instance, the velocity used to control the first workgroup electric actuator may be a velocity for performing the operation as commanded (e.g., a commanded velocity).
During controlled operation of the first workgroup electric actuators, the electronic processor 700 may determine a present electric current of the first workgroup electric actuator (at block 915). For example, the electronic processor 700 may determine the present electric current of the first workgroup electric actuator while the first workgroup electric actuator is controlled, via the velocity control parameter, to perform the operation. Accordingly, the present electric current of the first workgroup electric actuator may represent an electric current associated with performing the operation under a velocity control scheme. The electronic processor 700 may determine the present electric current of the first workgroup electric actuator based on an operator command or input associated with operating the power machine 600, sensed operation data associated with the power machine 600, or a combination thereof. For example, the electronic processor 700 may determine the present electric current of the first workgroup electric actuator based on electric current data or information collected by the workgroup electric current sensor(s) 668.
Continuing, the present electric current of the first workgroup electric actuator can then be used to determine a target electric current of the second workgroup electric actuator. For example, the present electric current of the first workgroup electric actuator (as determined at block 915) may be set as a target electric current for a second workgroup electric actuator of the set of workgroup electric actuators 660. The electronic processor 700 may then control the second workgroup electric actuator based on the target electric current to perform the operation (at block 920). Accordingly, in some configurations, the electronic processor 700 may implement an electric current control scheme for the second workgroup electric actuator, where the electric current control parameter used to control the second workgroup electric actuator is (or is determined based on) the present electric current (e.g., the target electric current) of the first workgroup electric actuator (e.g., as determined at block 915).
Therefore, according to the force balancing method of
As one example, an operator of the power machine 600 may provide a lift command for raising or lowering the lift arm 670 using a first electric lift actuator and a second electric lift actuator (e.g., as a set of electric lift actuators 675 configured to synchronously act on a common load, such as the lift arm 670). Responsive to receiving the lift command, the electronic processor 700 may control the first electric lift actuator based on a target velocity associated with the lift command (e.g., the velocity control parameter). The electronic processor 700 may then determine a present electric current of the first electric lift actuator during operation based on the velocity control parameter, and the present electric current of the first electric lift actuator may be utilized as a target electric current for a second electric lift actuator. The electronic processor 700 may thus use the target electric current (e.g., the present electric current of the first electric lift actuator) to control the second electric lift actuator (e.g., as an electric current control parameter). As such, by controlling the electric current of the second electric lift actuator to substantially match the electric current of the first electric lift actuator, the electronic processor 700 can substantially balance forces between the set of electric lift actuators 675 such that each electric lift actuator 675 exerts the same or substantially the same force on the common load (e.g., the lift arm 670).
Accordingly, in some configurations, the electronic processor 700 may control a first electric actuator in a velocity control scheme and a second electric actuator in an electric current control scheme. In particular, according to the force balancing method of
As illustrated in
The electronic processor 700 may determine a target velocity for the set of workgroup electric actuators 660 (at block 1010). The electronic processor 700 may determine the target velocity based on the received command (e.g., at block 1005). In some configurations, the target velocity is associated with a velocity for performing the commanded operation (e.g., a commanded velocity). The electronic processor 700 may then control the set of electric actuators based on the target velocity (at block 1015). For instance, the electronic processor 700 may adjust a control signal to the set of workgroup electric actuators 660, based on deviation of the electric actuators 660 from the target velocity. Accordingly, in some configurations, the electronic processor 700 may control the set of electric actuators using a velocity control parameter, where the velocity control parameter is associated with performing a commanded operation (e.g., the velocity control parameter is the target velocity).
While controlling the set of workgroup electric actuators 660 based on the target velocity, the electronic processor 700 may monitor electric currents of the set of workgroup electric actuators 660 (at block 1020). For instance, the electronic processor 700 may monitor an electric current for one of the workgroup electric actuators of the set of workgroup electric actuators 660 (e.g., a present electric current for a first workgroup electric actuator). Alternatively, the electronic processor 700 may monitor an electric current for each of the workgroup electric actuators included in the set of workgroup electric actuators 660. Accordingly, in some configurations, the electronic processor 700 may determine a present electric current for one or more of the workgroup electric actuators included in the set of workgroup electric actuators 660. The electronic processor 700 may determine a present electric current based on an operator command or input associated with operating the power machine 600, sensed operation data associated with the power machine 600 (e.g., electric current information collected via the workgroup electric current sensor(s) 668), etc.
To effect force balancing, in particular, the electronic processor 700 may monitor the electric currents of the set of workgroup electric actuators 660 in order to determine (or detect) an electric current difference between the electric currents for the electric actuators included in the set of workgroup electric actuators 660 (at block 1025). For example, the electronic processor 700 may determine a first present electric current for a first electric actuator and a second present electric current for a second electric actuator. The electronic processor 700 may then compare the first present electric current and the second electric current to determine an electric current difference. The electronic processor 700 may thus detect an electric current difference when the first present electric current and the second electric current are not the same or sufficiently similar. Accordingly, in some configurations, the electronic processor 700 may detect an electric current difference when the difference between electric currents (e.g., the first electric current and the second electric current) exceed a tolerance threshold (e.g., fall outside of an acceptable tolerance amount or range).
When an electric current difference is not detected (i.e., “No” at block 1025), the electronic processor 700 may repeat (or recursively perform) one or more of the illustrated operations of the method 1000. For example, when there is no electric current difference detected between the electric actuators of the set of workgroup electric actuators 660, the electronic processor 700 may continue to control the set of workgroup electric actuators 660 based on the target velocity (e.g., at block 1015), continue to monitor electric currents of the set of workgroup electric actuators 660 to detect electric current differences (e.g., at blocks 1020 and 1025), etc.
When an electric current difference is detected (i.e., “Yes” at block 1025), the electronic processor 700 may determine a set of adjusted target velocities (at block 1030) based on the electric current difference, and control one or more electric actuators of the set of workgroup electric actuators 660 based on the set of adjusted target velocities (at block 1035). In some configurations, the electronic processor 700 may determine an adjusted target velocity for each electric actuator included in the set of workgroup electric actuators 660 (e.g., a first adjusted target velocity for a first electric actuator, a second adjusted target velocity for a second electric actuator, etc.). Alternatively, the electronic processor 700 may determine an adjusted target velocity for a single electric actuator include din the set of workgroup electric actuators 660.
As noted above, the electronic processor 700 may determine an adjusted target velocity based on an electric current difference. Thus, for example, when an electric current difference is present, as may correspond to an undesired force imbalance, the target velocities of one or more of the actuators can be adjusted accordingly, to change the relative movement of the actuators and thereby reduce the current (and force) imbalance. As one example, for a first electric actuator, the electronic processor 700 may determine a change in velocity for the first electric actuator using the following equation: Change in Velocity=(Electric Current of Second Electric Actuator−Electric Current of First Electric Actuator)×Velocity Gain. The electronic processor 700 may then determine the adjusted target velocity for the first electric actuator based on the change in velocity (e.g., either increasing or decreasing the target velocity by the change in velocity). As another example, for a second electric actuator, the electronic processor 700 may determine a change in velocity for the second electric actuator using the following equation: Change in Velocity=(Electric Current of First Electric Actuator−Electric Current of Second Electric Actuator)×Velocity Gain. The electronic processor 700 may then determine the adjusted target velocity for the second electric actuator based on the change in velocity (e.g., either increasing or decreasing the target velocity by the change in velocity). Thus, for example, when the forces at the first electric actuator exceed the forces at the second electric actuator, a positive change in velocity may be commanded at the second electric actuator and a negative change in velocity may be commanded at the first electric actuator, so that the second electric actuator effectively catches up to the first electric actuator and the forces on the actuators are correspondingly brought more into balance.
In some configurations, the electronic processor 700 may determine an adjusted target velocity based on a velocity gain that is a function of the electric current difference. For example, a larger velocity gain may be applied when there is a larger force imbalance, as indicated by a larger electric current difference, and a smaller velocity gain may be applied when there is a smaller force imbalance, as indicated by a smaller electric current difference.
As illustrated in
In some configurations, the electronic processor 700 may repeat one or more operations of the method 1000 intermittently or periodically (e.g., at a predetermined frequency). For instance, in some configurations, the electronic processor 700 may periodically monitor the electric currents of the set of workgroup electric actuators 660 (at block 1020) to detect electric current differences (at block 1025) at a predetermined frequency, such as, e.g., at a pre-determined frequency of about 100 Hz.
Accordingly, in some configurations, the electronic processor 700 may implement force balancing between a set of workgroup electric actuators 660 to maintain a force of each electric actuator to be the same or substantially the same, as the set of electric actuators act on a load (e.g., the lift arm 670, the work element 655, etc.). According to the method 1000, the electronic processor 700 may (substantially) balance force between the set of workgroup electric actuators 660 by monitoring and adjusting individual target velocities for each respective workgroup electric actuator 660. For instance, for a first electric actuator, the electronic processor 700 may increase (e.g., speed up) or decrease (e.g., slow down) a target velocity for the first electric actuator depending on whether the electric current of the first electric actuator is above or below an electric current of another electric actuator (e.g., a second electric actuator positioned opposite the first electric actuator). Once an electric actuator is substantially matching the electric current of an opposite electric actuator, the electric actuator may follow the target velocity with small adjustments to the speed to maintain the forces substantially balanced (e.g., the same or substantially the same).
As illustrated in
The electronic processor 700 may determine a target electric current based on the command (at block 1110). For example, the electronic processor 700 may determine the target electric current based on a difference between a present velocity for the set of workgroup electric actuators 660 and a velocity corresponding to a commanded movement (e.g., the command received at block 1105). Alternatively, or in addition, the electronic processor 700 may determine the target electric current based on a difference between an average present velocity of the set of workgroup electric actuators 660 (or an electric actuator included therein) and a velocity corresponding to the commanded movement (e.g., the command received at block 1105). Generally, in this regard, the electronic processor 700 may employ real time position data from a motor to monitor a present operation of an actuator, with velocity and acceleration being readily determinable as first and second derivatives of the position, and with force and electric current being proportional to acceleration according to basic physical identities and the known operational characteristics of electric motors.
In some configurations, the electronic processor 700 may determine the target electric current based on an average present position of the set of workgroup electric actuators 660 (or an electric actuator included therein). For instance, the electronic processor 700 may receive position data (e.g., from the workgroup position sensor(s) 667) including a present position for each electric actuator included in the set of workgroup electric actuators 660. The electronic processor 700 may then determine an average present position, which the electronic processor 700 may use to determine the target electric current. In such configurations, the electronic processor 700 may convert (or otherwise transform) position information (e.g., the average present position) to relevant velocity information (e.g., by utilizing one or more physics identities).
As illustrated in
In some configurations, when zero velocity is commanded for the work element 655, the electronic processor 700 may determine a holding electric current (e.g., as the target electric current) for maintaining a present position or orientation for the set of workgroup electric actuators 660. In such configurations, the electronic processor 700 may provide the holding current to the set of workgroup electric actuators 660 (e.g., the first and second electric actuators) based on a target position or a target zero velocity.
Accordingly, in some configurations, the electronic processor 700 may implement force balancing between a set of workgroup electric actuators 660 to maintain a force of each electric actuator the same or substantially the same as the set of electric actuators act on a load (e.g., the lift arm 670, the work element 655, etc.). According to the method 1100, the electronic processor 700 may control (e.g., maintain) electric currents to be substantially similar or the same for each electric actuator included in the set of workgroup electric actuators 660 (e.g., providing the same commanded electric current to each electric actuator).
In some implementations of the force balancing control method of
Thus, examples of the disclosed systems and methods can provide for improved operation of sets of electric actuators for a power machine. For example, as further detailed above, cooperating sets of actuators can be controlled based on mixed or unified control schemes so that forces applied by the actuators are substantially balanced, with corresponding benefits for case and efficiency of operation and for actuator health and lifespan.
It is to be understood that the phraseology and terminology used herein is for the purpose of description and should not be regarded as limiting. The use of “including,” “comprising,” or “having” and variations thereof herein is meant to encompass the items listed thereafter and equivalents thereof as well as additional items. Further, unless otherwise noted, features or functionality of any particular example presented herein can be substituted into or otherwise combined with other examples, including to supplement or replace various features or functionality of the other examples.
Likewise, unless otherwise specified or limited, the terms “mounted,” “connected,” “supported,” and “coupled” and variations thereof are used broadly and encompass both direct and indirect mountings, connections, supports, and couplings. Further, unless otherwise specified or limited, “connected” and “coupled” are not restricted to physical or mechanical connections or couplings.
Unless otherwise specified or limited, the terms “about” and “approximately,” as used herein with respect to a reference value, refer to variations from the reference value of +20% or less (e.g., +15, +10%, +5%, etc.), inclusive of the endpoints of the range. Similarly, as used herein with respect to a reference value, the term “substantially equal” (and the like) refers to variations from the reference value of +5% or less (e.g., +2%, +1%, +0.5%) inclusive. Where specified in particular, “substantially” can indicate a variation in one numerical direction relative to a reference value. In particular, the term “substantially less” than a reference value (and the like) indicates a value that is reduced from the reference value by 30% or more (e.g., 35%, 40%, 50%, 65%, 80%), and the term “substantially more” than a reference value (and the like) indicates a value that is increased from the reference value by 30% or more (e.g., 35%, 40%, 50%, 65%, 80%). Thus, for example, “substantially balanced forces” and the like, with respect to two actuators, indicates that forces at a first of the actuators are within +5% (inclusive) of forces at a second of the actuators.
Also as used herein, unless otherwise limited or defined, “or” indicates a non-exclusive list of components or operations that can be present in any variety of combinations, rather than an exclusive list of components that can be present only as alternatives to each other. For example, a list of “A, B, or C” indicates options of: A; B; C; A and B; A and C; B and C; and A, B, and C. Correspondingly, the term “or” as used herein is intended to indicate exclusive alternatives only when preceded by terms of exclusivity, such as “either,” “one of,” “only one of,” or “exactly one of.” For example, a list of “one of A, B, or C” indicates options of: A, but not B and C; B, but not A and C; and C, but not A and B. A list preceded by “one or more” (and variations thereon) and including “or” to separate listed elements indicates options of one or more of any or all of the listed elements. For example, the phrases “one or more of A, B, or C” and “at least one of A, B, or C” indicate options of: one or more A; one or more B; one or more C; one or more A and one or more B; one or more B and one or more C; one or more A and one or more C; and one or more of A, one or more of B, and one or more of C. Similarly, a list preceded by “a plurality of” (and variations thereon) and including “or” to separate listed elements indicates options of multiple instances of any or all of the listed elements. For example, the phrases “a plurality of A, B, or C” and “two or more of A, B, or C” indicate options of: A and B; B and C; A and C; and A, B, and C.
In some implementations, devices or systems disclosed herein can be utilized, manufactured, installed, etc. using methods embodying aspects of the disclosed technology. Correspondingly, unless otherwise indicated, any description herein of particular features, capabilities, or intended purposes of a device or system should be considered to disclose, as examples of the disclosed technology a method of using such devices for the intended purposes, a method of otherwise implementing such capabilities, a method of manufacturing relevant components of such a device or system (or the device or system as a whole), and a method of installing disclosed (or otherwise known) components to support such purposes or capabilities. Similarly, unless otherwise indicated, discussion herein of any method of manufacturing or using for a particular device or system, including installing the device or system, should be understood to disclose, as examples of the disclosed technology, the utilized features and implemented capabilities of such device or system.
Some methods of the disclosed technology may be presented above or below with operations listed in a particular order. Unless otherwise required or specified, the operations of such methods can be implemented in different orders, in parallel, or as selected sub-sets of one or more individual operations (e.g., with a particular listed operation being implemented alone, rather than in combination with others).
Unless otherwise specifically indicated, ordinal numbers are used herein for convenience of reference, based generally on the order in which particular components are presented in the relevant part of the disclosure. In this regard, for example, designations such as “first,” “second,” etc., generally indicate only the order in which a thus-labeled component is introduced for discussion and generally do not indicate or require a particular spatial, functional, temporal, or structural primacy or order. Relatedly, similar or identical components may be referred to with different ordinal numbers in different contexts.
In some embodiments, aspects of the technology disclosed herein, including computerized implementations of methods according to the technology disclosed herein, can be implemented as a system, method, apparatus, or article of manufacture using standard programming or engineering techniques to produce software, firmware, hardware, or any combination thereof to control a processor device (e.g., a serial or parallel general purpose or specialized processor chip, a single- or multi-core chip, a microprocessor, a field programmable gate array, any variety of combinations of a control unit, arithmetic logic unit, and processor register, and so on), a computer (e.g., a processor device operatively coupled to a memory), or another electronically operated controller to implement aspects detailed herein. Accordingly, for example, embodiments of the technology disclosed herein can be implemented as a set of instructions, tangibly embodied on a non-transitory computer-readable media, such that a processor device can implement the instructions based upon reading the instructions from the computer-readable media. Some embodiments of the technology disclosed herein can include (or utilize) a control device such as an automation device, a special purpose or general purpose computer including various computer hardware, software, firmware, and so on, consistent with the discussion below. As specific examples, a control device can include a processor, a microcontroller, a field-programmable gate array, a programmable logic controller, logic gates etc., and other typical components that are known in the art for implementation of appropriate functionality (e.g., memory, communication systems, power sources, user interfaces and other inputs, etc.). In some embodiments, a control device can include a centralized hub controller that receives, processes and (re) transmits control signals and other data to and from other distributed control devices (e.g., an engine controller, an implement controller, a drive controller, etc.), including as part of a hub-and-spoke architecture or otherwise.
The term “article of manufacture” as used herein is intended to encompass a computer program accessible from any computer-readable device, carrier (e.g., non-transitory signals), or media (e.g., non-transitory media). For example, computer-readable media can include but are not limited to magnetic storage devices (e.g., hard disk, floppy disk, magnetic strips, and so on), optical disks (e.g., compact disk (CD), digital versatile disk (DVD), and so on), smart cards, and flash memory devices (e.g., card, stick, and so on). Additionally, it should be appreciated that a carrier wave can be employed to carry computer-readable electronic data such as those used in transmitting and receiving electronic mail or in accessing a network such as the Internet or a local area network (LAN). Those skilled in the art will recognize that many modifications may be made to these configurations without departing from the scope or spirit of the claimed subject matter.
Certain operations of methods according to the technology disclosed herein, or of systems executing those methods, may be represented schematically in the FIGS. or otherwise discussed herein. Unless otherwise specified or limited, representation in the FIGS. of particular operations in particular spatial order may not necessarily require those operations to be executed in a particular sequence corresponding to the particular spatial order. Correspondingly, certain operations represented in the FIGS., or otherwise disclosed herein, can be executed in different orders than are expressly illustrated or described, as appropriate for particular embodiments of the technology disclosed herein. Further, in some embodiments, certain operations can be executed in parallel, including by dedicated parallel processing devices, or separate computing devices configured to interoperate as part of a large system.
As used herein in the context of computer implementation, unless otherwise specified or limited, the terms “component,” “system,” “module,” “block,” and the like are intended to encompass part or all of computer-related systems that include hardware, software, a combination of hardware and software, or software in execution. For example, a component may be, but is not limited to being, a processor device, a process being executed (or executable) by a processor device, an object, an executable, a thread of execution, a computer program, or a computer. By way of illustration, both an application running on a computer and the computer can be a component. One or more components (or system, module, and so on) may reside within a process or thread of execution, may be localized on one computer, may be distributed between two or more computers or other processor devices, or may be included within another component (or system, module, and so on).
Although the technology disclosed herein has been described with reference to preferred embodiments, workers skilled in the art will recognize that changes may be made in form and detail to the disclosed embodiments without departing from the spirit and scope of the concepts discussed herein.
This application claims priority to U.S. Provisional Patent Application No. 63/580,063, filed Sep. 1, 2023, the entirety of which is incorporated by reference herein.
Number | Date | Country | |
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63580063 | Sep 2023 | US |