초록

A method for controlling autopilot roll capture of a rocket comprising adapting the start time and the rate of roll capture such that regardless of the initial rocket spin rate, the roll capture process is completed at a predetermined time.

대표청구항 ▼

1. A method for controlling autopilot roll capture of a rocket comprising: calculating a start time for de-spin of the rocket; andimplementing a rate of de-spin of the rocket such that regardless of an initial rocket spin rate, the roll capture process completes at a predetermined time based on the

1. A method for controlling autopilot roll capture of a rocket comprising: calculating a start time for de-spin of the rocket; andimplementing a rate of de-spin of the rocket such that regardless of an initial rocket spin rate, the roll capture process completes at a predetermined time based on the calculated start time and the implemented rate of de-spin. 2. The method of claim 1 wherein the implementing of the rate of de-spin is accomplished by adjusting an angle of a flaperon on the rocket. 3. The method of claim 1 further comprising adapting the spin rate by adjusting the angle of the flaperon on the rocket. 4. The method of claim 1 further comprising: determining that a current spin rate of the rocket is below a predetermined threshold; andclosing control loops for roll, pitch and yaw of the rocket in response to the determination. 5. The method of claim 1 wherein the predetermined roll capture completion time coincides with rocket motor burnout. 6. A method for controlling autopilot roll capture of a rocket comprising the steps, where T is current time, Wp is current spin rate, and Wpdot is spin rate deceleration: calculating a roll capture start time based on Wp, a selected Wpdot and a predetermined roll capture completion time;waiting for T to reach the calculated roll capture start time;implementing the selected Wpdot; andmonitoring Wp. 7. The method of claim 6 further comprising periodically adapting the Wp based on the monitoring to achieve the predetermined roll capture completion time. 8. The method of claim 6 further comprising closing control loops for roll, pitch and yaw of the rocket after Wp falls below a predetermined threshold. 9. The method of claim 6 wherein the selection of Wpdot is based on spin rate sensor constraints. 10. The method of claim 6 wherein a flaperon is deployed on the rocket at an angle necessary to achieve Wpdot. 11. The method of claim 6 wherein the method does not begin until T exceeds a predetermined minimum start time. 12. The method of claim 6 wherein the predetermined roll capture completion time coincides with rocket motor burnout. 13. An autopilot roll capture apparatus for a rocket comprising the steps, where T is current time, Wp is current spin rate, and Wpdot is spin rate deceleration: a processor to calculate a roll capture start time based on Wp, a selected Wpdot and a predetermined roll capture completion time;a timer to wait for T to reach the calculated roll capture start time;an implementation unit to achieve the selected Wpdot; anda sensor to monitor Wp. 14. The autopilot roll capture apparatus of claim 13 further comprising an adaptation unit to periodically adapt the Wp based on the monitoring to achieve the predetermined roll capture completion time. 15. The autopilot roll capture apparatus of claim 13 further comprising a control loop for yaw, pitch and roll of the rocket, to be closed after Wp falls below a predetermined threshold. 16. The autopilot roll capture apparatus of claim 13 further comprising a flaperon capable of being set to a continuously adjustable angle as necessary to achieve Wpdot. 17. The autopilot roll capture apparatus of claim 13 wherein the predetermined roll capture completion time coincides with rocket motor burnout.