Actively stabilized payload support apparatus and methods

• US 9,360,740 B2
• Filed: 05/01/2014
• Issued: 06/07/2016
• Est. Priority Date: 11/02/2011
• Status: Active Grant

• Current Assignee: Garrett W. Brown, Steven D. Wagner
• Original Assignee: Garrett W. Brown, Steven D. Wagner
• Inventors: Wagner, Steven D., Brown, Garrett W.
• Primary Examiner(s): Marc, McDieunel
• Application Number:
  US14/267,500
• Publication Number:
  US 20140288694A1
• Time in Patent Office: 768 Days
• Field of Search: 700/213, 700/245, 318/649, 701/2, G9B/27.01, G9B/27.033
• US Class Current: 1/1
• CPC Class Codes: F16M 11/105 the horizontal axis being the roll axis, e.g. for creating a landscape-portrait rotation
• CPC Class Codes: F16M 11/18 with mechanism for moving the apparatus relatively to the stand
• CPC Class Codes: F16M 11/2064 for tilting and panning F16M11/2078 takes precedence
• CPC Class Codes: F16M 13/00 Other supports for positioning apparatus or articles heads thereof F16M11/02 ; undercarriages thereof F16M11/20 ; adapted to be stuck in the ground A45F3/44 ; sockets or holders for poles or posts E04H12/22; Means for steadying hand-held apparatus or articles supports for measuring instruments G01D11/30; supports for casings of remote control switching devices H01H9/025
• CPC Class Codes: F16M 13/022 repositionable
• CPC Class Codes: F16M 13/04 for supporting on, or holding steady relative to, a person, e.g. by chains , e.g. rifle butt or pistol grip supports, supports attached to the chest or head apparatus or arrangements for taking photographs or for projecting or viewing them G03B
• CPC Class Codes: F16M 2200/042 for panning movement
• CPC Class Codes: F16M 2200/044 for balancing rotational movement of the undercarriage
• CPC Class Codes: G03B 17/561 Support related camera accessories

Abstract

A payload stabilizer suitable for use with video camera payloads. The stabilizer has a feedback system providing supplemental torques to the payload through a gimbal while remaining responsive to direct operator control.

Claims

1. A method of stabilizing a balanced component assembly having a plurality of torque generators, the method comprising:

(a) using one or more angular motion sensing units, measuring and providing angular rates and orientation motions of the balanced component assembly about three substantially mutually orthogonal axes, wherein such angular rates and orientation motions include that which is produced by operator input and external disturbances;

(b) providing a physical model comprising selected angular rates and orientation motions for the three substantially mutually orthogonal axes;

(c) comparing, using a signal processor, the measured angular rates and orientation motions to the modeled angular rates and orientation motions, respectively, for each of the three substantially mutually orthogonal axes, to create a comparison for each of the substantially mutually orthogonal axes;

(d) generating a supplemental torque signal for each of the substantially mutually orthogonal axes based on the respective comparisons derived in step (c);

(e) applying each of the supplemental torque signals to a respective torque generator;

(f) repeating step (a) through (e) to form a feedback loop.

2. The method of claim 1 comprising:

comparing, using a signal processor, the measured angular rates and orientation motions to the modeled angular rates and orientation motions, respectively, for each of the three substantially mutually orthogonal exes, using a separate algorithm for each of the substantially mutually orthogonal axes to create a comparison for each of the substantially mutually orthogonal axes.

3. The method of stabilizing a balanced component assembly of claim 1 wherein the three mutually orthogonal axes correspond to pan, tilt and roll.

4. The method of stabilizing a balanced component assembly of claim 1 wherein the measured angular rates and orientation motions provided by the angular motion sensing unit are vehicle referenced, the method further comprising:

converting the vehicle-referenced angular rates and orientation motion to earth-referenced angular rates and orientation motion using an artificial horizon algorithm.

5. The method of stabilizing a balanced component assembly of claim 1 wherein the supplemental torque signal increases the angular inertia of the rig.

6. The method of stabilizing a balanced component assembly of claim 3 further comprising:

adding static torque and frictional torque referenced to a fixed inertial frame to the modeled tilt torque and modeled pan torque of the physical model.

7. The method of stabilizing a balanced component assembly of claim 1 wherein the moment of inertia and coefficient of dynamic braking friction are automatically reduced over time as a function of increasing measured angular rate about each substantially mutually orthogonal axis.

8. The method of stabilizing a balanced component assembly of claim 7 further comprising;

providing a threshold torque below a supplemental torque limit;

reducing the supplemental torque when external torque reaches the threshold torque; and

re-applying supplemental torque when the external torque departs from the threshold torque.

9. The method of stabilizing a balanced component assembly of claim 1 wherein the operator input includes torque applied remotely to the omni-axial torque generator by an operator.

10. The method of stabilizing a balanced component assembly of claim 1 wherein:

when the tilt axis angle equals an angle in a selected range, a roll axis leveling algorithm prevails; and

when the tilt axis angle departs from the selected range, an inertial only algorithm prevails.

11. The method of stabilizing a balanced component assembly of claim 10 wherein the selected tilt axis angle range is about +/−

80°

.

12. The method of stabilizing a balanced component assembly of claim 4 wherein:

when the tilt axis angle equals a threshold angle a pan axis algorithm is modified to be increasingly responsive to a vehicle-referenced angular rate and orientation motion of the pan axis.

13. The method of claim 1:

wherein the plurality of torque generators include a roll generator and a tilt generator;

wherein the supplemental torque signals include a supplemental tilt torque value and a supplemental roll torque value;

the method further comprising;

providing a counter programmed to track a pan shaft angle representing the momentary angular position of a yoke of the gimbal as momentary relationships of the gimbal torques vary;

calculating torques to be generated by a roll motor and a tilt motor based on the supplemental tilt torque value, the supplemental roll torque value and the pan shaft angle; and

applying signals to the roll and tilt torque generators based on the calculated torques.

14. An apparatus for stabilizing a payload comprising:

a rig having a gimbal;

the gimbal having an omni-axial torque generator;

the omni-axial torque generator comprising a roll torque generator, a tilt torque generator and a pan torque generator;

a feedback controller;

the omni-axial torque generator driven by a supplemental torque output signal generated by the feedback controller;

an angular motion sensing unit capable of measuring angular rates and orientation motions produced by the omni-torque generator wherein the angular rates and orientation motions include that which is produced by external disturbances;

the feedback controller having a signal processor functionally connected to the angular motion sensing unit to receive as an input the measured rates and measured orientations;

the signal processor including;

an artificial horizon algorithm;

a first axis algorithm;

a second axis algorithm; and

a third pan axis algorithm;

the signal processor, by the respective algorithms, capable of processing the measured angular rates and orientation motions to produce the supplemental torque signals to be applied to each of the first, second and third axes, which when applied modify the angular rates and angular orientations to conform to a physical model.

15. The apparatus of claim 14 comprising an operator-control surface for controlling motion about the second axis and the third axis, wherein motion about the first axis is controlled by the feedback controller only.

16. The apparatus of claim 14 comprising:

a handle assembly;

the handle assembly having a shell rotatable about a hollow third torque generator shaft;

a motor fixedly attached to the third torque generator shaft;

wires disposed within the third torque generator shaft and connected to the motor;

a top end cap freely rotatable about the third torque generator shaft while fixedly engaged to the shell;

a bottom end cap fixedly engaged to the shell bottom end, the bottom end cap having a hole therein in which third torque generator is disposed and fixedly attached;

the arrangement allowing the shell to be substantially unlimitedly rotatable about the third axis output shaft without twisting the wires.

17. The apparatus of claim 14 wherein the omni-axial torque generator generates torque about the first, second and third axes, which are mutually orthogonal and correspond to pan, tilt and roll.

18. The apparatus of claim 14 wherein the algorithms add static torque and frictional torque referenced to a fixed inertial frame to the modeled second torque and modeled third torque of the physical model.

19. The apparatus of claim 14 comprising a remotely controlled omni-axial torque generator controlled by operator input.

20. The apparatus claim 14 further comprising a passive-trans-gimbal coupling, wherein the passive-trans-gimbal coupling provides additional external torque.

21. The apparatus of claim 14 further comprising:

a pan-axis counter programmed to track the proportion between variations in sum and direction of gimbal torques with respect to two of the axes, the two axes corresponding to roll and tilt.

22. A method of stabilizing a balance component assembly having a pan shaft and a gimbal, the gimbal having a yoke and a plurality of torque generators, the torque generators including a roll motor and a tilt motor, the method comprising:

providing a supplemental tilt torque value;

providing a supplemental roll torque value;

providing a counter around a pan axis programmed to track a pan axis angle representing the momentary angular position of the gimbal yoke as the momentary relationships of the gimbal torques vary;

calculating torques to be generated by the roll motor and tilt motor based on the supplemental tilt torque value, the supplemental roll torque value and the pan shaft angle; and

applying signals to the pan and tilt torque generators based on the calculated torques.

23. The method of claim 22 wherein the relative percentage and direction of torque required for tilt motors compared to yoke roll motors is continuously influence.