Two-axis mirror stabilization assembly

• US 4,881,800 A
• Filed: 05/16/1988
• Issued: 11/21/1989
• Est. Priority Date: 05/16/1988
• Status: Expired due to Term

• Current Assignee: Gec-Marconi Electronics Systems Corporation
• Original Assignee: Plessey Electronics Systems Corporation
• Inventors: Volpe, Joseph J., Kass, Jordan S., Heckathorn, David L., Lindsay, Peter, Haessig, David A. Jr., Fuchs, Charles R.
• Primary Examiner(s): Bovernick, Rodney B.
• Assistant Examiner(s): Shafer, R. D.
• Application Number:
  US07/194,367
• Time in Patent Office: 554 Days
• Field of Search: 350/500, 354/70, 354/72, 358/222, 73/504, 244/175, 364/453, 74/5.22, 74/5.6 R, 74/5 R
• US Class Current: 359/555
• CPC Class Codes: G02B 27/64 Imaging systems using optical elements for stabilisation of the lateral and angular position of the image
• CPC Class Codes: Y10T 74/1218 Combined

Abstract

To stabilize the line-of-sight of an optical image relative to a commanded line-of-sight, a stabilization system consisting of a mirror having two limited degrees of freedom, a two axis gyroscope having its two sensitive axes perpendicular to the LOS, a pickoff sensor feeding back mirror angular position, servo compensators that provide mirror torque commands to a two axis mirror torquer, and the electronic hardware that ties these components together is used.

Claims

1. In an optical stabilizing system having an assembly for tracking a command line of sight and rejecting environmental perturbations, the line of sight being chosen in accordance with an input command signal, the assembly comprising:

a mirror;

a rigid block;

means flexibly coupling the mirror to the rigid block, the flexible coupling means providing two axes of freedom for the mirror;

gyroscopic means mounted to the rigid block, the spin axis of the gyroscopic means being aligned along the line of sight, the gyroscopic means providing a gyro rate signal about two axes perpendicular to the line of sight;

means for torquing the mirror;

means for sensing the movement of the mirror and providing a feedback pickoff signal corresponding thereto; and

control means for receiving the command signal, the gyro rate signal and the feedback pickoff signal and, based on these signals, providing a torquer signal to the torquing means for torquing the mirror;

whereby the torquer signal is responsive for cancelling the environmental perturbations and torques the mirror only to track the command line of sight.

2. The assembly according to claim 1, wherein the flexible coupling means comprises a flexure hinge having movement about two axes.

3. The assembly according to claim 1, wherein the rigid block is secured to gimbals and is part of an image capture and display system for a vehicle.

4. The assembly according to claim 1, wherein the torquing means comprises at least a pair of torquer coils, and wherein the sensing means comprises a plurality of pickoff coils.

5. The assembly according to claim 1, wherein the control means comprises at least one compensator circuit for converting the command signal, the gyro rate signal and the feedback pickoff signal into a plurality of estimated states to be used to generate the output torquer signal, the estimated states including parameters to match the environmental perturbations, wherein the estimated states comprise a pickoff angle corresponding to the position of the mirror relative to a base, a high frequency rate for the vehicle to which the assembley is mounted, a gimbal rate relative to the vehicle, a high frequency position for the vehicle, a high frequency disturbance variable, a low frequency rate for the vehicle and an inertial rate of the mirror.

6. The assembly according to claim 5, wherein the control means further comprises a torque limiter connected to the compensator circuit for receiving the torquer signal, the torque limiter confining the magnitude of the torquer signal within predetermined levels so as to prevent the mirror from being torqued excessively.

7. The assembly according to claim 1, wherein the command signal is provided as an input from a helmet worn by a pilot and wherein the line of sight moves in accordance with the movement of the helmet.

8. The assembly according to claim 1, wherein the control means comprises compensator circuits for elevation and azimuth axes perpendicular to the command line of sight, both elevation and azimuth compensator circuits generating torquer signals for torquing the mirror along the elevation and azimuth axes.

9. The assembly according to claim 8, wherein the measurement of the respective elevation and azimuth axes are fed to the corresponding compensator circuit;

and

wherein each output torquer signal is a sum of a plurality of estimated states provided as outputs from the corresponding compensator circuit and multiplied with a plurality of gain coefficients.

10. The assembly according to claim 1, wherein the mirror torquing means comprises.

means for amplifying the torquer signals;

means for filtering the amplified torquer signal;

means for maintaining a particular amplitude for the amplified torquer signal;

means for processing the amplified torquer signal; and

means for using the processed torquer signal to drive torquer coils in the assembly for maintaining the mirror in its null position. thereby rejecting the environmental perturbations.

11. In an optical stabilizing system having an assembly including a mirror, a method of torquing the mirror to track a command line of sight relative to a moving reference and to track the moving reference and to reject environmental perturbations, the method comprising the steps of:

flexibly coupling the mirror to a rigid block so as to provide two axes of freedom for the mirror;

mounting a gyroscopic means to the rigid block;

stabilizing the line of sight relative to an input command signal;

aligning the spin axis of the gyroscopic means along the line of sight, thereby enabling the gyroscopic means to provide a gyro rate signal about two axes perpendicular to the line of sight;

sensing the movement of the mirror and providing a feedback signal corresponding thereto;

transforming the input command signal, the gyro rate signal and the feedback signal into a plurality of estimated states;

combining the estimated states to produce an output torquer signal responsive to canceling the environmental perturbations and tracking the line of sight; and

torquing the mirror in accordance to the torquer signal to track the command and stabilize line of sight.

12. The method according to claim 11, further comprising the step of securing the rigid block to gimbals to form an image capture and display system for a vehicle.

13. The method according to claim 11, wherein the transforming step further comprises the step of:

transfer functioning the input command, gyro rate and feedback signals into the following estimated states;

(a) a pickoff angle corresponding to the position of the mirror relative to a base;

(b) a high frequency rate for the vehicle on which the assembly is mounted to;

(c) a gimbal rate relative to the vehicle;

(d) a high frequency position for the vehicle;

(e) a high frequency disturbance variable;

(f) a low frequency rate for the vehicle; and

(g) an inertial rate of the mirror.

14. The method according to claim 13, further comprising the step of:

limiting the magnitude of the torquer signal to prevent the mirror from being excessively torqued and to provide a compensator with torque information consistent with the actual torque applied.

15. The method according to claim 11, wherein the transforming step further comprises the steps of:

generating estimated measurement signals; and

subtracting the estimated measurement signals from the input command, gyro rate and feedback signals to produce residual signals.

16. The method according to claim 15, further comprising the steps of:

multiplying the residual signals with a plurality of gain coefficients to generate a plurality of correction terms;

using the correction terms to generate a plurality of corrected estimate states; and

multiplying the corrected estimate states with corresponding gain coefficients to generate the torquer signal.

17. The method according to claim 11, wherein the torquing step further comprises:

maintaining the mirror in its null position, environmental perturbations notwithstanding, to track the command line of sight.