Patent Application
20190265731
The present invention generally relates to equipment for aircraft operations, and more particularly relates to an apparatus and method for providing enhanced autopilot mode awareness for a pilot of an aircraft.
Various studies and surveys of flight crews use of autopilot systems note that pilots routinely encountered so-called automation surprises. Automation surprises are situations that prompt pilots to ask about the autopilot system: “What is it doing?”; “Why is it doing that?”; and “What will it do next?”. These concerns associated with automation surprises are of particular concern in general aviation contexts where single pilot operations, and lower experience levels compound the situation. Hence, there is a need for an autopilot system that not only provides information allowing pilots to anticipate the effects of various autopilot modes, but also to see the targets being held by an autopilot system in operation.
This summary is provided to describe select concepts in a simplified form that are further described in the Detailed Description. This summary is not intended to identify key or essential features of the claimed subject matter, nor is it intended to be used as an aid in determining the scope of the claimed subject matter.
An apparatus is provided for providing enhanced autopilot mode awareness for a pilot of an aircraft. The apparatus comprises: an autopilot control interface that allows the pilot to activate an operational mode of an autopilot system for the aircraft and to set aviation function parameters of the autopilot system; and an autopilot status interface that displays, the operational mode of the autopilot system, a current status of the aviation function parameters that are controlled by the autopilot system, and an indicator of anticipated actions by the autopilot system to control the aviation function parameters.
A method is provided for providing enhanced autopilot mode awareness for a pilot of an aircraft. The method comprises: activating an autopilot system for the aircraft using an autopilot control interface that allows the pilot to activate an operational mode for the autopilot system; setting an aviation function parameter target for the autopilot system with the autopilot control interface; displaying, with an autopilot status interface, the operational mode of the autopilot system, a preview of the aviation function parameter target, a current status of the aviation function parameter target that is controlled by the autopilot system, an indicator of anticipated actions by the autopilot system to achieve the aviation function parameter target, and supplemental cues showing progress toward achieving the aviation function parameter target.
Furthermore, other desirable features and characteristics of the apparatus and method will become apparent from the subsequent detailed description and the appended claims, taken in conjunction with the accompanying drawings and the preceding background.
The present invention will hereinafter be described in conjunction with the following drawing figures, wherein like numerals denote like elements, and wherein:
The following detailed description is merely exemplary in nature and is not intended to limit the invention or the application and uses of the invention. As used herein, the word “exemplary” means “serving as an example, instance, or illustration.” Thus, any embodiment described herein as “exemplary” is not necessarily to be construed as preferred or advantageous over other embodiments. All of the embodiments described herein are exemplary embodiments provided to enable persons skilled in the art to make or use the invention and not to limit the scope of the invention which is defined by the claims. Furthermore, there is no intention to be bound by any expressed or implied theory presented in the preceding technical field, background, brief summary, or the following detailed description.
An apparatus for providing enhanced autopilot mode awareness for a pilot of an aircraft has been developed. The apparatus has an autopilot control interface that allows the pilot to place the autopilot system in an operational mode and set aviation function parameters for the aircraft. The apparatus also includes an autopilot status interface that displays the operational mode of the autopilot system, the current status of the aviation function parameters that are being controlled by the autopilot system and an indicator of the anticipated actions by the autopilot system to control the aircraft in accordance with the aviation function parameters.
The autopilot display allows the pilot to preview targets that will be acquired and held by the autopilot system should a given mode be engaged. The display will provide supplemental cues in the form of text, icons, aural signals, or other cues to make anticipated aircraft behavior clear to the pilot prior to mode engagement. Once a mode is engaged, the autopilot would show any active aircraft parameters being acquired and or held. Supplemental cues will show progress towards the acquisition of the target by the autopilot system.
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In these examples, the autopilot system is shown to control such aviation function parameters as flight direction, pitch and roll of the aircraft, and altitude selection. However, it should be understood that other flight parameters for the aircraft may be controlled by the autopilot system. For example, vertical flight parameters such as a pitch angle function that maintains the pitch attitude of the aircraft may be included. Additionally, an altitude hold function that maintains a present altitude of the aircraft and an airspeed hold function that maintains a specific airspeed for the aircraft may be included. Lateral flight parameters may also be controlled in other embodiments including a heading hold function that maintains a specific heading of the aircraft and a navigation hold function that maintains a specific navigation point for the aircraft.
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Those of skill in the art will appreciate that the various illustrative logical blocks, modules, circuits, and algorithm steps described in connection with the embodiments disclosed herein may be implemented as electronic hardware, computer software, or combinations of both. Some of the embodiments and implementations are described above in terms of functional and/or logical block components (or modules) and various processing steps. However, it should be appreciated that such block components (or modules) may be realized by any number of hardware, software, and/or firmware components configured to perform the specified functions. To clearly illustrate this interchangeability of hardware and software, various illustrative components, blocks, modules, circuits, and steps have been described above generally in terms of their functionality. Whether such functionality is implemented as hardware or software depends upon the particular application and design constraints imposed on the overall system. Skilled artisans may implement the described functionality in varying ways for each particular application, but such implementation decisions should not be interpreted as causing a departure from the scope of the present invention. For example, an embodiment of a system or a component may employ various integrated circuit components, e.g., memory elements, digital signal processing elements, logic elements, look-up tables, or the like, which may carry out a variety of functions under the control of one or more microprocessors or other control devices. In addition, those skilled in the art will appreciate that embodiments described herein are merely exemplary implementations.
The various illustrative logical blocks, modules, and circuits described in connection with the embodiments disclosed herein may be implemented or performed with a general purpose processor, a digital signal processor (DSP), an application specific integrated circuit (ASIC), a field programmable gate array (FPGA) or other programmable logic device, discrete gate or transistor logic, discrete hardware components, or any combination thereof designed to perform the functions described herein. A general-purpose processor may be a microprocessor, but in the alternative, the processor may be any conventional processor, controller, microcontroller, or state machine. A processor may also be implemented as a combination of computing devices, e.g., a combination of a DSP and a microprocessor, a plurality of microprocessors, one or more microprocessors in conjunction with a DSP core, or any other such configuration.
The steps of a method or algorithm described in connection with the embodiments disclosed herein may be embodied directly in hardware, in a software module executed by a processor, or in a combination of the two. A software module may reside in RAM memory, flash memory, ROM memory, EPROM memory, EEPROM memory, registers, hard disk, a removable disk, a CD-ROM, or any other form of storage medium known in the art. An exemplary storage medium is coupled to the processor such that the processor can read information from, and write information to, the storage medium. In the alternative, the storage medium may be integral to the processor. The processor and the storage medium may reside in an ASIC. The ASIC may reside in a user terminal. In the alternative, the processor and the storage medium may reside as discrete components in a user terminal
In this document, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Numerical ordinals such as “first,” “second,” “third,” etc. simply denote different singles of a plurality and do not imply any order or sequence unless specifically defined by the claim language. The sequence of the text in any of the claims does not imply that process steps must be performed in a temporal or logical order according to such sequence unless it is specifically defined by the language of the claim. The process steps may be interchanged in any order without departing from the scope of the invention as long as such an interchange does not contradict the claim language and is not logically nonsensical.
Furthermore, depending on the context, words such as “connect” or “coupled to” used in describing a relationship between different elements do not imply that a direct physical connection must be made between these elements. For example, two elements may be connected to each other physically, electronically, logically, or in any other manner, through one or more additional elements.
While at least one exemplary embodiment has been presented in the foregoing detailed description of the invention, it should be appreciated that a vast number of variations exist. It should also be appreciated that the exemplary embodiment or exemplary embodiments are only examples, and are not intended to limit the scope, applicability, or configuration of the invention in any way. Rather, the foregoing detailed description will provide those skilled in the art with a convenient road map for implementing an exemplary embodiment of the invention. It being understood that various changes may be made in the function and arrangement of elements described in an exemplary embodiment without departing from the scope of the invention as set forth in the appended claims.
