The present invention pertains to carriers, such as trailers, that may be attached to a balancing transporter and, more particularly, to an attachment mechanism that permits tilting action of the balancing transporter.
Dynamically balancing transporters refer to personal vehicles having a motion control system that actively maintains the stability of the transporter while the transporter is operating. The motion control system maintains the stability of the transporter by continuously sensing the orientation of the transporter, determining any corrective action to maintain stability, and commanding the wheel motors to make the corrective action. One such transporter is described in U.S. Pat. No. 6,302,230. Other dynamically balancing transporters are described in U.S. Pat. Nos. 5,701,965 and 5,971,091. Each of these patents is incorporated by reference herein in its entirety.
While control systems for balancing transporters can respond to certain extraneous torques, the torque presented by a trailer coupled to a balancing transporter in an arbitrary manner would vary nonlinearly with the orientation of the transporter and would present an obstacle to stable control of the transporter.
In embodiments of the present invention, a carrier is pivotally attached to a dynamically balancing transporter with a hitch. The axis of the hitch's pivotal attachment to the transporter is made coincident with the rotational axis of the transporter's wheels. Thus, the hitch exerts zero torque about the rotational axis of the wheel minimizing the impact to the dynamic balance of the transporter.
In a specific embodiment of the invention, the carrier is attached to the transporter such that the carrier is disposed behind the transporter. In another embodiment of the invention, the carrier is disposed in front of the transporter.
In another embodiment of the invention, a chain of balancing transporters and carriers is provided. A given transporter or carrier is pivotally attached to the carrier or transporter immediately in front of and behind the given transporter or carrier. The pivot axis of any connection to a balancing transporter in the chain is made coincident with the rotational axis of the transporter's wheels. In this way, the impact on the dynamic balance of each transporter is minimized.
The foregoing features of the invention will be more readily understood by reference to the following detailed description, taken with reference to the accompanying drawings, in which:
Definitions: as used in this description and the accompanying claims, the following terms shall have the meanings indicated, unless the context otherwise requires:
A “wheel” is any ground contacting member that is capable of rotation on an axis.
A “carrier” is any platform that is capable of carrying a payload which is suspended on at least one wheel. Carriers include, without limitation, trailers, carts (whether preceding or following an attached transporter) and even other transporters. A carrier may be powered or unpowered.
A “fore-aft plane” will mean a plane that is perpendicular to the rotational axis of a ground contacting element and that contains a vertical line thru a point of ground contact of the ground contacting element. The term “lateral plane” will mean a plane that is parallel to the rotational axis of a ground contacting element and that contains a vertical line thru a point of ground contact of the ground contacting element
A “dynamically balancing (or balanced) transporter” will mean a transporter that lacks static stability in at least a fore-aft plane.
An alternative to operation of a statically stable transporter is that dynamic stability may be maintained by action of the user, as in the case of a bicycle or motorcycle or scooter, or, in accordance with embodiments of the present invention, by a control loop, as in the case of the human transporter described in U.S. Pat. No. 5,701,965. The invention may be implemented in a wide range of embodiments. A characteristic of many of these embodiments is the use of a pair of laterally disposed wheels to suspend the subject over the surface with respect to which the subject is being transported. The ground or other surface, such as a floor, over which a transporter in accordance with the invention is employed may be referred to generally herein as the “ground.” The wheels are typically motor-driven. In many embodiments, the configuration in which the subject is suspended during locomotion lacks inherent stability at least a portion of the time with respect to a vertical in the fore-aft plane but is relatively stable with respect to a vertical in the lateral plane. Stability, as defined below, means that in response to a perturbation a stable device will tend towards its unperturbed state.
In various embodiments of a balancing transporter, fore-aft stability may be achieved by providing a control loop, in which one or more motors are included, for operation of a motorized drive in connection with the wheels. In these embodiments, the wheels are driven by the motorized drive in the control loop in such a way as to maintain, when the transporter is not in locomotion, the center of mass of the transporter above the region of contact of the wheels with the ground, regardless of disturbances and forces operative on the transporter.
A wheel typically has a “point” (actually, a region) of contact or tangency with the surface over which the transporter is traveling or standing. Due to the compliance of the wheel, the “point” of contact is actually an area, where the region of contact may also be referred to as a contact patch. The weight of the transporter is distributed over the contact region, giving rise to a distribution of pressures over the region, with the center of pressure displaced forward during forward motion. The distribution of pressures is a function both of the composition and structure of the wheel, the rotational velocity of the wheel, the torque applied to the wheel, and thus of the frictional forces acting on the wheel.
A force in the direction of motion is required to overcome rolling friction (and other frictional forces, including air resistance). Gravity may be used, in accordance with preferred embodiments of the invention, to provide a torque about the point of contact with the surface in a direction having a component in the sense of desired motion. Referring to
The wheel is driven with respect to the transporter by a torque T (supplied by a motor, for example) which in turn creates a reaction torque—T on the transporter. Since the torque acts about the axle 164, the reaction torque corresponds to a force Fb acting at the center of gravity (CG) of the system, including the transporter and payload, where Fb=T/RCG, where RCG is the distance between the axle and the CG of the system. The line 170 from the CG to point P is at an angle θs relative to the vertical 172.
The rolling friction, f, acting on the wheel at point P, is proportional to the velocity v of the rim of the wheel, with the proportionality expressed as f=μv. For constant velocity to be maintained, this force f must be exactly canceled. Consequently, with gravity providing the force, the condition that must be satisfied is:
Fb cos θs=fb, (Eqn. 1)
where fb is the component of the reaction force acting transverse to axis 174 between the CG and point P. In order to prevent the transporter from falling, a stability condition must also exist, namely that no net force acts on the CG in a direction transverse to line 170, i.e., there is no net torque about the point of contact P during motion at constant velocity (i.e., in an inertial frame of reference where the point P is fixed). This condition may be expressed as:
Fg sin θs=fb, (Eqn. 2)
where Fg sin θs is the “tipping” component of gravity, and fb is the counter-tipping component of the reactive force on the transporter caused by wheel rotation (fb=Fb cos θ), and where θ is the angle shown line 170 and line 174.
Eqns. 1 and 2 may be combined to yield Fg sin θs cos θs=f=μv, thus, in the limit of small angles (where sin θ is approximately θ),
θs=(μ/Fg)v, (Eqn. 3)
showing that increasing velocity requires increased lean to overcome the effects of friction. Additionally, a control loop that imposes stability on the system will respond to an increased lean by increasing velocity of the system. While the preceding discussion assumed constant velocity, additional lean beyond that required to overcome the effects of friction will result in acceleration since an additional forward-directed force acts on the CG. Conversely, in order to achieve acceleration (or deceleration) of the transporter, additional leaning (forward or backward) must be provided in a manner discussed in further detail below.
Operation of the balancing transporter will be described with reference to the set of coordinate axes shown in
A simplified control algorithm for achieving balance in the embodiment of the invention according to
T=K1(θ−θ0)+K2({dot over (θ)}={dot over (θ)}0)+K3(x−x0)+K4({dot over (x)}−{dot over (x)}0) (Eqn. 4)
where:
T denotes a torque applied to a wheel about its axis of rotation;
θ is a quantity corresponding to the lean of the entire system about the ground contact, with θ0 representing the magnitude of a system pitch offset, all as discussed in detail below;
x identifies the fore-aft displacement along the surface relative to a fiducial reference point, with x0 representing the magnitude of a specified fiducial reference offset;
a dot over a character denotes a variable differentiated with respect to time; and
a subscripted variable denotes a specified offset that may be input into the system as described below; and
K1, K2, K3, and K4 are gain coefficients that may be configured, either in design of the system or in real-time, on the basis of a current operating mode and operating conditions as well as preferences of a user. The gain coefficients may be of a positive, negative, or zero magnitude, affecting thereby the mode of operation of the vehicle, as discussed below. The gains K1, K2, K3, and K4 are dependent upon the physical parameters of the system and other effects such as gravity. The simplified control algorithm of
The effect of θ0 in the above control equation (Eqn. 4) is to produce a specified offset θ0 from the non-pitched position where θ=0. Adjustment of θ0 will adjust the vehicle's offset from a non-pitched position. As discussed in further detail below, in various embodiments, pitch offset may be adjusted by the user, for example, by means of a thumb wheel 32, shown in
The size of K3 will determine the extent to which the transporter will seek to return to a given location. With a non-zero K3, the effect of x0 is to produce a specified offset −x0 from the fiducial reference by which x is measured. When K3 is zero, the transporter has no bias to return to a given location. The consequence of this is that if the transporter is caused to lean in a forward direction, the transporter will move in a forward direction, thereby maintaining balance. Such a configuration is discussed further below.
The term “lean” is often used with respect to a system balanced on a single point of a perfectly rigid member. In that case, the point (or line) of contact between the member and the underlying surface has zero theoretical width. In that case, furthermore, lean may refer to a quantity that expresses the orientation with respect to the vertical (i.e., an imaginary line passing through the center of the earth) of a line from the center of gravity (CG) of the system through the theoretical line of ground contact of the wheel. While recognizing, as discussed above, that an actual wheel is not perfectly rigid, the term “lean” is used herein in the common sense of a theoretical limit of a rigid wheel. The term “system” refers to all mass caused to move due to motion of the wheels with respect to the surface over which the transporter is moving.
“Stability” as used in this description and in any appended claims refers to the mechanical condition of an operating position with respect to which the system will naturally return if the system is perturbed away from the operating position in any respect.
Acceleration of the transporter may be established by system lean. For example, to achieve forward acceleration of the transporter by forward system lean; the center of gravity of the system (transporter and payload) would be placed forward of the center of the pressure distribution of the contact region where the wheels contact the ground—the more the lean, the more the acceleration. Thus, furthermore, it can be seen that leaning, in conjunction with gravity and friction, determines acceleration (positive or negative) of the system. In this manner, if the transporter is moving forward, pitching the system back will achieve braking. Because the transporter must overcome friction, there is typically some system lean when the transporter is moving at constant velocity over level ground. In other words, looking at the torque on the transporter caused by gravity and the torque caused by all other external forces, the torque applied by the motorized drive is adjusted so that the net torque from all these sources produces a desired acceleration.
As described above, dynamic stability for a transporter can be maintained by applying a torque to a wheel about its axis of rotation. Attachment of a carrier to the transporter may be advantageous to increase the payload carrying capacity of the transporter. Such attached carriers must not impact substantially the dynamic stability of the transporter. Generally speaking, any component of a force exerted by the carrier on the transporter that is transverse to the vertical direction must be minimized or particularly accounted for by the control law.
In an embodiment of the present invention a carrier is pivotally attached to a dynamically balancing transporter with a hitch. The axis of the hitch's pivotal attachment to the transporter is made coincident with the rotational axis of the transporter's wheels. The hitch exerts zero torque about the rotational axis of the wheel thereby minimizing the impact to the dynamic balance and control of the transporter.
Referring to
Referring to
In another embodiment of the invention, the trailer hitch is attached to the transporter inboard of the transporter's wheels, as shown in
In other embodiments of the present invention, any number of carriers or balancing transporters may be attached to each other in a chain of carriers or transporters. The attachment of one transporter or carrier to the adjacent transporter or carrier is with a hitch that includes a fore-aft pivot. At each pivotal hitch connection to a balancing transporter, the axis of the fore-aft pivot is made coincident with the rotational axis of the transporter's wheels. This attachment scheme minimizes the effect of the attached carrier or transporter on the balance and control of the transporter to which it is attached.
In another embodiment of the invention, as shown in
The described embodiments of the invention are intended to be merely exemplary and numerous variations and modifications will be apparent to those skilled in the art. While the preceding embodiments have been described in terms of use of one or more Wheels as a ground contacting element for the transporter and for the carrier(s), other types of ground contacting elements may be employed in embodiments of the invention. The various types of ground contacting elements may be mixed in any combination in various embodiments of the invention. These and other variations and modifications are intended to be within the scope of the present invention as defined in the appended claims.
The present application is a continuation-in-part of copending application Ser. No. 10/164,333, filed Jun. 05, 2002 now abandoned which is a divisional application of application Ser. No. 09/516,384, filed Mar. 1, 2000 now U.S. Pat. No. 6,435,535 both of which are incorporated herein by reference in their entirety.
Number | Name | Date | Kind |
---|---|---|---|
584127 | Draullette et al. | Jun 1897 | A |
849270 | Schafer et al. | Apr 1907 | A |
1739716 | Fisher | Dec 1929 | A |
2742973 | Johannesen | Apr 1956 | A |
3145797 | Taylor | Aug 1964 | A |
3260324 | Suarez | Jul 1966 | A |
3283398 | Andren | Nov 1966 | A |
3288234 | Feliz | Nov 1966 | A |
3348518 | Forsyth et al. | Oct 1967 | A |
3374845 | Selwyn | Mar 1968 | A |
3399742 | Malick | Sep 1968 | A |
3446304 | Alimanestiano | May 1969 | A |
3450219 | Fleming | Jun 1969 | A |
3515401 | Gross | Jun 1970 | A |
3580344 | Floyd | May 1971 | A |
3596298 | Durst, Jr. | Aug 1971 | A |
3724874 | Simpson | Apr 1973 | A |
3860264 | Douglas et al. | Jan 1975 | A |
3872945 | Hickman et al. | Mar 1975 | A |
3952822 | Udden et al. | Apr 1976 | A |
4018440 | Deutsch | Apr 1977 | A |
4062558 | Wasserman | Dec 1977 | A |
4076270 | Winchell | Feb 1978 | A |
4088199 | Trautwein | May 1978 | A |
4094372 | Notter | Jun 1978 | A |
4109741 | Gabriel | Aug 1978 | A |
4111445 | Haibeck | Sep 1978 | A |
4151892 | Francken | May 1979 | A |
4222449 | Feliz | Sep 1980 | A |
4264082 | Fouchey, Jr. | Apr 1981 | A |
4266627 | Lauber | May 1981 | A |
4293052 | Daswick et al. | Oct 1981 | A |
4325565 | Winchell | Apr 1982 | A |
4354569 | Eichholz | Oct 1982 | A |
4363493 | Veneklasen | Dec 1982 | A |
4373600 | Buschbom et al. | Feb 1983 | A |
4375840 | Campbell | Mar 1983 | A |
4510956 | King | Apr 1985 | A |
4560022 | Kassai | Dec 1985 | A |
4566707 | Nitzberg | Jan 1986 | A |
4570078 | Yashima et al. | Feb 1986 | A |
4571844 | Komasaku et al. | Feb 1986 | A |
4624469 | Bourne, Jr. | Nov 1986 | A |
4645230 | Hammons | Feb 1987 | A |
4657272 | Davenport | Apr 1987 | A |
4685693 | Vadjunec | Aug 1987 | A |
4709772 | Brunet | Dec 1987 | A |
4716980 | Butler | Jan 1988 | A |
4740001 | Torleumke | Apr 1988 | A |
4746132 | Eagan | May 1988 | A |
4770410 | Brown | Sep 1988 | A |
4786069 | Tang | Nov 1988 | A |
4790400 | Sheeter | Dec 1988 | A |
4790548 | Decelles et al. | Dec 1988 | A |
4794999 | Hester | Jan 1989 | A |
4798255 | Wu | Jan 1989 | A |
4802542 | Houston et al. | Feb 1989 | A |
4809804 | Houston et al. | Mar 1989 | A |
4834200 | Kajita | May 1989 | A |
4863182 | Chern | Sep 1989 | A |
4867188 | Reid | Sep 1989 | A |
4869279 | Hedges | Sep 1989 | A |
4874055 | Beer | Oct 1989 | A |
4890853 | Olson | Jan 1990 | A |
4919225 | Sturges | Apr 1990 | A |
4953851 | Sherlock et al. | Sep 1990 | A |
4984754 | Yarrington | Jan 1991 | A |
4985947 | Ethridge | Jan 1991 | A |
4998596 | Miksitz | Mar 1991 | A |
5002295 | Lin | Mar 1991 | A |
5011170 | Forbes et al. | Apr 1991 | A |
5011171 | Cook | Apr 1991 | A |
5052237 | Reimann | Oct 1991 | A |
5064209 | Kurschat | Nov 1991 | A |
5111899 | Reimann | May 1992 | A |
5158493 | Morgrey | Oct 1992 | A |
5161820 | Vollmer | Nov 1992 | A |
5168947 | Rodenborn | Dec 1992 | A |
5171173 | Henderson et al. | Dec 1992 | A |
5186270 | West | Feb 1993 | A |
5221883 | Takenaka et al. | Jun 1993 | A |
5240266 | Kelley et al. | Aug 1993 | A |
5241875 | Kochanneck | Sep 1993 | A |
5248007 | Watkins et al. | Sep 1993 | A |
5314034 | Chittal | May 1994 | A |
5350033 | Kraft | Sep 1994 | A |
5366036 | Perry | Nov 1994 | A |
5376868 | Toyoda et al. | Dec 1994 | A |
5419624 | Adler et al. | May 1995 | A |
5641173 | Cobb, Jr. | Jun 1997 | A |
5655615 | Mick | Aug 1997 | A |
5701965 | Kamen et al. | Dec 1997 | A |
5701968 | Wright-Ott et al. | Dec 1997 | A |
5718534 | Neuling | Feb 1998 | A |
5775452 | Patmont | Jul 1998 | A |
5791425 | Kamen et al. | Aug 1998 | A |
5794730 | Kamen | Aug 1998 | A |
5873582 | Kaufman et al. | Feb 1999 | A |
5921844 | Hollick | Jul 1999 | A |
5947505 | Martin | Sep 1999 | A |
5971091 | Kamen et al. | Oct 1999 | A |
5973463 | Okuda et al. | Oct 1999 | A |
5975225 | Kamen et al. | Nov 1999 | A |
5986221 | Stanley | Nov 1999 | A |
6003624 | Jorgensen et al. | Dec 1999 | A |
6039142 | Eckstein et al. | Mar 2000 | A |
6050357 | Staelin et al. | Apr 2000 | A |
6059062 | Staelin et al. | May 2000 | A |
6125957 | Kauffmann | Oct 2000 | A |
6131057 | Tamaki et al. | Oct 2000 | A |
6223104 | Kamen et al. | Apr 2001 | B1 |
6225977 | Li | May 2001 | B1 |
6288505 | Heinzmann et al. | Sep 2001 | B1 |
6302230 | Kamen et al. | Oct 2001 | B1 |
6312001 | Boyer | Nov 2001 | B1 |
6435535 | Field et al. | Aug 2002 | B1 |
20020063006 | Amesbury et al | May 2002 | A1 |
Number | Date | Country |
---|---|---|
2 048 593 | May 1971 | DE |
31 28 112 | Feb 1983 | DE |
32 42 880 | Jun 1983 | DE |
3411489 | Oct 1984 | DE |
44 04 594 A 1 | Aug 1995 | DE |
196 25 498 C 1 | Nov 1997 | DE |
298 08 091 | Oct 1998 | DE |
298 08 096 | Oct 1998 | DE |
0 109 927 | Jul 1984 | EP |
0 193 473 | Sep 1986 | EP |
0 537 698 | Apr 1993 | EP |
0663 313 | Jul 1995 | EP |
0 958 978 | Nov 1999 | EP |
980 237 | May 1951 | FR |
2 502 090 | Mar 1982 | FR |
152664 | Feb 1922 | GB |
1213930 | Nov 1970 | GB |
2 139 576 | Nov 1984 | GB |
52-44933 | Oct 1975 | JP |
57-87766 | Jun 1982 | JP |
57-110569 | Jul 1982 | JP |
59-73372 | Apr 1984 | JP |
62-12810 | Jul 1985 | JP |
0255580 | Dec 1985 | JP |
61-31685 | Feb 1986 | JP |
63-305082 | Dec 1988 | JP |
2-190277 | Jul 1990 | JP |
4-201793 | Jul 1992 | JP |
6-171562 | Dec 1992 | JP |
5-213240 | Aug 1993 | JP |
6-105415 | Dec 1994 | JP |
7255780 | Mar 1995 | JP |
WO 8605752 | Oct 1986 | WO |
WO 8906117 | Jul 1989 | WO |
WO 9623478 | Aug 1996 | WO |
WO 9846474 | Oct 1998 | WO |
WO 00 75001 | Dec 2000 | WO |
Number | Date | Country | |
---|---|---|---|
20040129464 A1 | Jul 2004 | US |
Number | Date | Country | |
---|---|---|---|
Parent | 09516384 | Mar 2000 | US |
Child | 10164333 | US |
Number | Date | Country | |
---|---|---|---|
Parent | 10164333 | Jun 2002 | US |
Child | 10626468 | US |