Torque control for balloon coupling
Aspects of the disclosure provide for controlling orientation of a payload of a balloon through a despin mechanism. In one instance, a system may include a flexible coupling configured to reduce effects of a balloon envelope tilting on a payload, a sensor configured to measure rotational displacement of the flexible coupling, a despin mechanism including a motor configured to rotate the payload, and a controller. The controller may be configured to use receive the measured rotational displacement and to use the despin mechanism to rotate the payload towards a preferred orientation based on the measured rotational displacement.
1. A system comprising:
a flexible coupling connecting a balloon envelope to a payload;
a despin mechanism including a motor configured to rotate the payload; and
a controller operatively associate with the despin mechanism to rotate the payload towards a preferred orientation based on movements of said flexible coupling.
2. The system of claim 1 , wherein the payload includes a solar panel, and the preferred orientation corresponds to the solar panel being oriented towards the sun.
3. The system of claim 1 , wherein the payload includes a communications system, and the preferred orientation corresponds to the communications system being oriented in a particular direction to send and receive information with a network target.
4. The system of claim 1 , wherein the flexible coupling includes a first end and a second end, and wherein a sensor is configured to measure rotational displacement between the first end and the second end.
5. The system of claim 4 , wherein the controller is further configured to control the despin mechanism based on the amount of torque in order to attempt to maintain zero torque at the flexible coupling.
6. The system of claim 4 , wherein the sensor is a magnetic encoder.
7. The system of claim 4 , wherein the sensor is an optical encoder.
8. The system of claim 4 , wherein the sensor is a potentiometer.
9. The system of claim 4 , wherein the sensor is a strain gauge.
10. The system of claim 1 , further comprising a thermometer configured to measure temperature of the flexible coupling, and wherein the controller is further configured to operate the despin mechanism further based on the temperature measurement.
11. The system of claim 1 , further comprising a thermometer configured to measure ambient temperature near the flexible coupling, and wherein the controller is further configured to operate the despin mechanism further based on the ambient temperature.
12. A method of orienting a payload of a balloon, the method comprising:
interconnecting the payload to the balloon with a flexible coupling;
identifying, by a controller, a preferred orientation of the payload;
determining, by the controller, a control action based on movement of the flexible coupling; and
sending, by the controller, a signal to a despin mechanism to cause the despin mechanism to rotate the payload according to the control action and towards the identified preferred orientation of the payload.
13. The method of claim 12 , further comprising receive, by the controller, orientation information from an orientation sensor identifying a current orientation of the payload, and wherein the control action is determined further based on the received orientation information.
14. The method of claim 12 , wherein determining the control action includes determining an amount of torque based.
15. The method of claim 14 , wherein the amount of torque is determined based on stiffness of the flexible coupling.
16. The method of claim 15 , further comprising:
receiving temperature information from a thermometer; and
using the temperature information to determine the stiffness of the flexible coupling, and wherein the amount of torque is determined further based on the determined stiffness.
17. The method of claim 16 , wherein the temperature is a temperature of the flexible coupling.
18. The method of claim 12 , further comprising, controlling the despin mechanism in order to attempt to maintain zero torque at the flexible coupling.