Gimbal radial counterbalance systems and methods

1. A system comprising:

a radial counterbalance mechanism comprising a counterbalance weight and a motor configured to adjust a radial position of the counterbalance weight relative to a rotational axis of a gimbal ring;

an orientation sensor configured to provide an orientation of a payload coupled to the gimbal ring, a platform coupled to the gimbal ring, and/or the gimbal ring; and

a logic device configured to communicate with the radial counterbalance mechanism and the orientation sensor, wherein the logic device is configured to:

receive the orientation of the payload, the platform, and/or the gimbal ring,

determine a compensating radial weight position for the counterbalance weight based, at least in part, on the received orientation, wherein the compensating radial weight position is configured to reduce a radial displacement of a center of gravity of the payload from the rotational axis of the gimbal ring, and

control the motor to position the counterbalance weight at the compensating radial weight position.

2. The system of claim 1 , wherein:

the orientation sensor comprises a first orientation sensor;

the radial counterbalance mechanism comprises a second orientation sensor configured to provide an orientation of the counterbalance weight; and

the logic device is configured to:

receive a current orientation of the counterbalance weight before controlling the motor to position the counterbalance weight at the compensating radial weight position;

determine a rotation direction for the motor based, at least in part, on the current orientation and the compensating radial weight position; and

control the motor to position the counterbalance weight at the compensating radial weight position and according to the determined rotation direction.

3. The system of claim 1 , wherein:

the radial counterbalance mechanism comprises a motor coupling configured to couple the motor to the counterbalance weight; and

the radial counter balance mechanism is coupled to the platform and/or the gimbal ring.

4. The system of claim 1 , wherein:

the radial counterbalance mechanism comprises a motor coupling configured to couple the motor to the counterbalance weight; and

the motor coupling comprises a planetary gear set or a worm drive comprising a lever arm and/or a cam configured to translate rotational motion of the motor into positions of the counterbalance weight along a counterbalance path determined, at least in part, by the lever arm and/or cam; and

the compensating radial weight position lies on the counterbalance path.

5. The system of claim 1 , wherein:

the radial counterbalance mechanism is configured to translate rotational motion of the motor into positions of the counterbalance weight along a planar counterbalance path; and

the planar counterbalance path lies in a plane perpendicular to the rotational axis of the gimbal ring.

6. The system of claim 5 , wherein:

the planar counterbalance path comprises a circular counterbalance path.

7. The system of claim 1 , wherein:

the received orientation comprises an absolute orientation of the payload and/or the gimbal ring relative to gravity; and

the logic device is configured to determine the compensating radial weight position for the counterbalance weight based, at least in part, on the absolute orientation of the payload and/or the gimbal ring.

8. The system of claim 1 , wherein:

the platform comprises a mobile platform;

the received orientation comprises a first orientation of the mobile platform and a second orientation of the payload and/or the gimbal ring; and

the logic device is configured to determine the compensating radial weight position for the counterbalance weight based, at least in part, on the first orientation of the mobile platform and the second orientation of the payload and/or the gimbal ring.

9. The system of claim 8 , further comprising an accelerometer configured to provide an acceleration of the mobile platform, wherein the logic device is configured to:

receive the acceleration of the mobile platform from the accelerometer; and

determine the compensating radial weight position for the counterbalance weight based, at least in part, on the first orientation of the mobile platform, the second orientation of the payload and/or the gimbal ring, and the acceleration of the mobile platform.

10. The system of claim 1 , wherein the payload comprises an articulated sensor comprising an imaging module configured to provide still and/or video images along a line of sight of the payload, wherein the logic device is configured to:

receive the video images along the line of sight of the payload from the imaging module;

determine a jitter amplitude and/or frequency in the received video images; and

adjust the compensating radial weight position for the counterbalance weight to reduce the jitter amplitude and/or frequency in the received video images.

11. A method comprising:

receiving an orientation of a payload coupled to a gimbal ring, a platform coupled to the gimbal ring, and/or the gimbal ring;

determining a compensating radial weight position for a counterbalance weight of a radial counterbalance mechanism based, at least in part, on the received orientation, wherein the compensating radial weight position is configured to reduce a radial displacement of a center of gravity of the payload from a rotational axis of the gimbal ring, and

controlling a motor of the radial counterbalance mechanism to position the counterbalance weight at the compensating radial weight position.

12. The method of claim 11 , wherein the radial counterbalance mechanism comprises an orientation sensor configured to provide an orientation of the counterbalance weight, the method further comprising:

receiving a current orientation of the counterbalance weight before controlling the motor to position the counterbalance weight at the compensating radial weight position;

determining a rotation direction for the motor based, at least in part, on the current orientation and the compensating radial weight position; and

controlling the motor to position the counterbalance weight at the compensating radial weight position and according to the determined rotation direction.

13. The method of claim 11 , wherein:

the radial counterbalance mechanism comprises a motor coupling configured to couple the motor to the counterbalance weight; and

the radial counter balance mechanism is coupled to the platform and/or the gimbal ring.

14. The method of claim 11 , wherein:

the radial counterbalance mechanism comprises a motor coupling configured to couple the motor to the counterbalance weight; and

the motor coupling comprises a planetary gear set or a worm drive comprising a lever arm and/or a cam configured to translate rotational motion of the motor into positions of the counterbalance weight along a counterbalance path determined, at least in part, by the lever arm and/or cam; and

the compensating radial weight position lies on the counterbalance path.

15. The method of claim 11 , wherein:

the radial counterbalance mechanism is configured to translate rotational motion of the motor into positions of the counterbalance weight along a planar counterbalance path; and

the planar counterbalance path lies in a plane perpendicular to the rotational axis of the gimbal ring.

16. The method of claim 15 , wherein:

the planar counterbalance path comprises a circular counterbalance path.

17. The method of claim 11 , wherein:

the received orientation comprises an absolute orientation of the payload and/or the gimbal ring relative to gravity; and

the determining the compensating radial weight position for the counterbalance weight is based, at least in part, on the absolute orientation of the payload and/or the gimbal ring.

18. The method of claim 11 , wherein:

the platform comprises a mobile platform;

the received orientation comprises a first orientation of the mobile platform and a second orientation of the payload and/or the gimbal ring; and

the determining the compensating radial weight position for the counterbalance weight is based, at least in part, on the first orientation of the mobile platform and the second orientation of the payload and/or the gimbal ring.

19. The method of claim 18 , further comprising:

receiving an acceleration of the mobile platform from an accelerometer; and

determining the compensating radial weight position for the counterbalance weight based, at least in part, on the first orientation of the mobile platform, the second orientation of the payload and/or the gimbal ring, and the acceleration of the mobile platform.

20. The method of claim 11 , wherein the payload comprises an articulated sensor comprising an imaging module configured to provide still and/or video images along a line of sight of the payload, the method further comprising:

receiving the video images along the line of sight of the payload from the imaging module;

determining a jitter amplitude and/or frequency in the received video images;

receiving a vibration amplitude and/or frequency of the platform from an accelerometer coupled to the platform;

determining the vibration amplitude and/or frequency correlates with the jitter amplitude and/or frequency; and

adjusting the compensating radial weight position for the counterbalance weight to reduce the jitter amplitude and/or frequency in the received video images.