Methods and systems for efficiently orienting an agile vehicle using a gyroscope array

• US 8,209,070 B2
• Filed: 12/17/2008
• Issued: 06/26/2012
• Est. Priority Date: 12/17/2008
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Hamilton, Brian
• Primary Examiner(s): Keith, Jack
• Assistant Examiner(s): Khatib, Rami
• Application Number:
  US12/337,304
• Publication Number:
  US 20100152953A1
• Time in Patent Office: 1,287 Days
• Field of Search: 701/3, 701/4, 701/5, 701/13, 701/14, 244/158.4, 244/158.6, 244/164, 244/165, 244/171, 244/175, 244/179
• US Class Current: 701/13
• CPC Class Codes: B64G 1/244 Spacecraft control systems
• CPC Class Codes: B64G 1/286 using control momentum gyroscopes (CMGs)

Abstract

Methods and systems are provided for orienting an agile vehicle using a control moment gyroscope array. A method comprises obtaining initial vehicle parameters for the vehicle and obtaining target vehicle parameters for the vehicle. The method further comprises determining command parameters based on a difference between the target vehicle parameters and the initial vehicle parameters, and simulating operation of the control moment gyroscope array using the command parameters and a torque value being at least equal to a maximum achievable torque for the control moment gyroscope array. When the simulated vehicle parameters are substantially equal to the target vehicle parameters, the method further comprises determining a torque profile for the control moment gyroscope array based on the simulated operation and operating the control moment gyroscope array using the torque profile.

Claims

1. A method for orienting a vehicle using a control moment gyroscope array, the method comprising:

obtaining initial vehicle parameters for the vehicle;

obtaining target vehicle parameters for the vehicle;

determining command parameters based on a difference between the target vehicle parameters and the initial vehicle parameters;

simulating operation of the control moment gyroscope array using the command parameters with a first torque value to obtain simulated vehicle parameters, the first torque value being at least equal to a maximum achievable torque for the control moment gyroscope array;

determining a torque profile for the control moment gyroscope array based on the simulated operation when the simulated vehicle parameters are substantially equal to the target vehicle parameters; and

operating the control moment gyroscope array using the torque profile.

2. The method of claim 1, further comprising:

determining that the simulated vehicle parameters are not substantially equal to the target vehicle parameters;

adjusting the command parameters based on the difference between the simulated vehicle parameters and the target vehicle parameters, wherein adjusting the command parameters results in adjusted command parameters; and

simulating operation of the control moment gyroscope array using the adjusted command parameters with the first torque value to obtain simulated vehicle parameters.

3. The method of claim 2, wherein adjusting the command parameters comprises adjusting the command parameters based on the difference between the simulated vehicle parameters and the target vehicle parameters using an iteration method.

4. The method of claim 1, wherein:

initial vehicle parameters comprise a first attitude and a first rotational rate;

target vehicle parameters comprise a target attitude and a target rotational rate; and

determining command parameters comprises determining command parameters based on the difference between the target attitude and the first attitude and the difference between the first rotational rate and the target rotational rate.

5. The method of claim 1, the target vehicle parameters having a target time, wherein determining command parameters comprises:

determining an acceleration torque direction;

determining a deceleration torque direction; and

determining a deceleration time, the deceleration time being chosen before the target time.

6. The method of claim 5, wherein simulating operation of the control moment gyroscope array comprises:

simulating operation of the control moment gyroscope array using a first torque command before the deceleration time, the first torque command comprising the first torque value in the acceleration torque direction; and

simulating operation of the control moment gyroscope array using a second torque command after the deceleration time, the second torque command comprising the first torque value in the deceleration torque direction.

7. The method of claim 5, further comprising:

determining that the simulated vehicle parameters are not substantially equal to the target vehicle parameters;

adjusting the command parameters based on the difference between the simulated vehicle parameters and the target vehicle parameters, wherein adjusting the command parameters results in an adjusted acceleration torque direction, an adjusted deceleration torque direction, and an adjusted deceleration time;

simulating operation of the control moment gyroscope array using a third torque command before the adjusted deceleration time, the third torque command comprising the first torque value in the adjusted acceleration torque direction; and

simulating operation of the control moment gyroscope array using a fourth torque command after the adjusted deceleration time, the fourth torque command comprising the first torque value in the adjusted deceleration torque direction.

8. The method of claim 7, wherein adjusting the command parameters comprises adjusting the command parameters based on the difference between the simulated vehicle parameters and the target vehicle parameters using an iteration method.

9. The method of claim 1, wherein simulating operation of the control moment gyroscope array comprises simulating operation of the control moment gyroscope array based on the command parameters and the first torque value using a steering control law.

10. The method of claim 9, wherein:

simulating operation of the control moment gyroscope array using the steering control law produces a resulting torque profile; and

determining the torque profile comprises storing the resulting torque profile.

11. A method for controlling an attitude of an agile vehicle using a plurality of gyroscopes, the agile vehicle having an initial attitude, the method comprising:

obtaining a target attitude for the agile vehicle at a target time;

determining a first torque direction based on a difference between the target attitude and the initial attitude;

simulating operation of the plurality of gyroscopes with a first torque value in the first torque direction, the first torque value being greater than or equal to a maximum achievable torque for the plurality of gyroscopes, wherein simulating operation of the plurality of gyroscopes results in a simulated attitude for the agile vehicle at the target time; and

determining rate commands for each gyroscope of the plurality of gyroscopes when the simulated attitude is substantially equal to the target attitude, wherein the plurality of gyroscopes are commanded using the rate commands to control the attitude of the agile vehicle.

12. The method of claim 11, the agile vehicle having an initial rotational velocity, the method further comprising obtaining a target rotational velocity for the agile vehicle at the target time wherein:

determining the first torque direction comprises determining the first torque direction based on a difference between the target rotational velocity and the initial rotational velocity;

simulating operation of the plurality of gyroscopes results in a simulated rotational velocity for the agile vehicle at the target time; and

determining rate commands comprises determining rate commands for each gyroscope of the plurality of gyroscopes if the simulated rotational velocity is substantially equal to the target rotational velocity.

13. The method of claim 12, further comprising:

determining a deceleration torque direction; and

determining a deceleration time, the deceleration time being chosen before the target time.

14. The method of claim 13, wherein simulating operation of the plurality of gyroscopes comprises:

simulating operation of the plurality of gyroscopes using a first torque command before the deceleration time, the first torque command comprising the first torque value in the first torque direction; and

simulating operation of the plurality of gyroscopes using a second torque command after the deceleration time, the second torque command comprising the first torque value in the deceleration torque direction.

15. The method of claim 14, wherein if the simulated rotational velocity is not substantially equal to the target rotational velocity, the method further comprises repeating the steps of:

iteratively adjusting the first torque direction, the deceleration torque direction, and the deceleration time based on a difference between the simulated rotational velocity and the target rotational velocity, wherein adjusting the first torque direction, the deceleration torque direction, and the deceleration time results in an adjusted first torque direction, an adjusted deceleration torque direction, and an adjusted deceleration time;

simulating operation of the plurality of gyroscopes using a third torque command before the adjusted deceleration time, the third torque command comprising the first torque value in the adjusted first torque direction; and

simulating operation of the plurality of gyroscopes using a fourth torque command after the adjusted deceleration time, the fourth torque command comprising the first torque value in the adjusted deceleration torque direction.

16. The method of claim 11, wherein if the simulated attitude is not substantially equal to the target attitude, the method further comprises:

adjusting the first torque direction based on a difference between the simulated attitude and the target attitude, wherein adjusting the first torque direction results in an adjusted first torque direction;

simulating operation of the plurality of gyroscopes with the first torque value in the adjusted first torque direction, wherein simulating operation of the plurality of gyroscopes results in an adjusted simulated attitude for the agile vehicle at the target time; and

determining rate commands for each gyroscope of the plurality of gyroscopes if the adjusted simulated attitude is substantially equal to the target attitude, wherein the plurality of gyroscopes are commanded using the rate commands to control the attitude of the agile vehicle.

17. The method of claim 16, wherein adjusting the first torque direction comprises iteratively adjusting the first torque direction based on a difference between the simulated attitude and the target attitude.

18. An attitude control system for an agile vehicle, the attitude control system comprising:

a gyroscope array, the gyroscope array comprising a plurality of control moment gyroscopes, the gyroscope array having a maximum achievable torque;

a communication module configured to receive target vehicle parameters;

a sensor system configured to obtain initial vehicle parameters for the agile vehicle;

a control module coupled to the communication module, the sensor system, and the communication module, wherein the control module is configured to;

determine first command parameters based on a difference between the target vehicle parameters and the initial vehicle parameters;

determine simulated vehicle parameters based on simulated operation of the gyroscope array using the first command parameters with a first torque value, the first torque value being greater than or equal to the maximum achievable torque;

determine a torque profile for the gyroscope array based on the simulated operation when the simulated vehicle parameters are substantially equal to the target vehicle parameters; and

operate the gyroscope array using the torque profile.

19. The attitude control system of claim 18, wherein the control module is configured to:

adjust the first command parameters based on the difference between the simulated vehicle parameters and the target vehicle parameters if the simulated vehicle parameters are not substantially equal to the target vehicle parameters, wherein adjusting the command parameters results in second command parameters; and

determine simulated vehicle parameters based on simulated operation of the gyroscope array using the second command parameters with the first torque value.

20. The attitude control system of claim 18, wherein the simulated operation of the gyroscope array using the first command parameters comprises:

simulating operation of the gyroscope array with the first torque value in an initial torque direction before a first time; and

simulating operation of the gyroscope array with the first torque value in a deceleration torque direction after the first time.