State-deviation-estimation circuit employing a phase-locked-loop phase reference

• US 4,791,573 A
• Filed: 09/02/1986
• Issued: 12/13/1988
• Est. Priority Date: 09/02/1986
• Status: Expired due to Term

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Sanders Associates, INC. (BAE Systems Plc)
• Inventors: Smith, Kirby A., Zemany, Paul D., Smith, John A.
• Primary Examiner(s): NOT, DEFINED
• Application Number:
  US06/902,815
• Time in Patent Office: 833 Days
• Field of Search: 364/453, 364/454, 364/459, 244/3.2, 244/3.21
• US Class Current: 701/221
• CPC Class Codes: G05D 1/108 animated with a rolling movement

Abstract

A system (34) for determining deviations in the state of motion of a projectile (10) from its intended state includes a comparison module (38) that receives the outputs S of a sensor array (36). The comparison module (38) converts the sensor outputs to a measurement vector Z_m and computes the deviation of this measurement vector from an intended measurement vector Z₀ received from a control system. The comparison module (38) then determines the difference E_Z between this measured deviation and the deviation predicted by a Kalman filter (44, 46). In generating the measurement vector Z_m from the outputs of the sensor array (36), the comparison module (38) "de-spins" the array outputs in accordance with the output of a phase reference (42), whose purpose is to indicate the phase with respect to gravity of the spin of the projectile (10) about its longitudinal axis. The Kalman filter'"'"'s state-deviation estimator (46) weights the vector output of the comparison module (36) and adds it to the output of the Kalman filter'"'"'s state-deviation predictor (44) to provide an updated state-deviation estimation E_X (t:t), which the state-deviation predictor (44) then uses as a basis for its next cycle. The output of the comparison module (38) constitutes a measure of the performance of the state-deviation predictor (44) and is used as a correction factor for the phase reference (42) so that the system acts as a phase-locked loop to lock the phase reference (42) onto the projectile spin without the need for an external sensor to determine the direction of gravity.

Claims

1. In a projectile for executing ballistic motion under the influence of gravity, a guidance system for guiding the projectile in accordance with a target-vector indication supplied thereto, the guidance system comprising:

A. a movable control surface on the projectile for affecting the motion of the projectile in accordance with the orientation of the control surface;

B. a sensor array for sensing enough physical quantities to determine predetermined kinematic variables if the spin orientation of the platform with respect to gravity is known and for generating a sensor outlet representative of the sensed quantities;

C. computation means, connected to receive the sensor output and adapted for reception of the target-vector indication, for;

(i) establishing a phase reference representing an estimate of the spin phase of the platform with respect to gravity;

(ii) employing a mathematical model of the platform to calculate a predicted state deviation from an indication of the previous state deviation and to produce a predicted-deviation indication that represents the predicted state deviation;

(iii) producing from the sensor output, the predicted-deviation indication, and the target-vector indication a difference output representing the difference between (a) the deviation, from the values indicated by the target-vector indication, of the kinematic variables derived from the sensor array in accordance with the phase reference and (b) the deviation, derived from the predicted-deviation indication, of the kinematic variables from the values indicated by the target vector;

(iv) generating from the predicted-deviation indication and the difference output an estimated-deviation output consisting of the predicted-deviation indication adjusted in accordance with the difference output to represent the new deviation in the state of the platform and using the estimated-deviation output as the indication of the previous state deviation in the next calculation of the predicted state deviation; and

(v) minimizing any misalignment of the phase reference with the direction of gravity by adjusting the phase reference in accordance with a component of the difference indication that results from misalignment of the phase reference with the direction of gravity, whereby the phase reference tends to be alignment with the force of gravity without the need for additional sensors; and

D. a direction-control system for moving the control surface so as to control its orientation in accordance with the estimated deviation output.

2. An apparatus as defined in claim 1 wherein the computation means:

A. produces correlation values by correlating successive periods of the sensor output with the phase reference;

B. generates a measurement vector by subjecting the correlation values to a transformation that results in a measurement vector having the proper values of the kinematic variables in the absence of sensor noise if the phase reference correctly represents the phase of rotation the platform with respect to gravity; and

C. generates the difference output by subtracting from the measurement vector the target vector and the deviation in the kinematic variables as derived from the predicted-deviation indication.

3. An apparatus as defined in claim 2 wherein:

A. the kinematic variables are different from the state variables in the predicted-deviation indication; and

B. the computation means converts the predicted-deviation indication to the kinematic variables derived therefrom before subtracting the derived kinematic variables from the measurement vector.

4. An apparatus as defined in claim 3 wherein the computation means produces a first difference by subtracting the target vector from the measurement vector and subtracts from the first difference the kinematic variables as derived from the predicted deviation.

5. An apparatus as defined in claim 4 wherein:

A. the kinematic variables are the translational accelerations in two axes perpendicular to the platform trajectory and rotational velocities about those two axes; and

B. the predicted deviation is the deviation in a state whose elements are the translational velocities in two axes perpendicular to the platform trajectory and the angular velocities about those two axes.

6. An apparatus as defined in claim 3 wherein:

A. the kinematic variables are the translational accelerations in two axes perpendicular to the platform trajectory and the rotational velocities about those two axes; and

B. the predicted deviation is the deviation in a state whose elements are the translational velocities in two axes perpendicular to the platform trajectory and the angular velocities about those two axes.

7. An apparatus as defined in claim 2 wherein:

A. the kinematic variables are the translational acceleration along a first axis perpendicular to gravity and to the platform trajectory, the translational acceleration along a second axis perpendicular to the first axis and to the platform trajectory, and the rotational velocities about the first and second axes; and

B. the computation means adjusts the phae reference in accordance with the element of the difference indication that corresponds to the translational acceleration along the first axis.

8. An apparatus as defined in claim 7 wherein the predicted deviation is the deviation in a state whose elements are the translational velocities in two axes perpendicular to the platform trajectory and the angular velocities about those two axes.

9. An apparatus as defined in claim 1 wherein the computation means:

A. produces an adjustment vector by converting the difference output to a state deviation and weighting it by a predetermined amount in comparison with the predicted deviation; and

B. adds the adjustment vector to the predicted deviation to produce the estimated-deviation output.

10. An apparatus as defined in claim 9 wherein the computation means weights the difference output in a direction favored by modeling errors.

11. An apparatus as defined in claim 10 wherein:

A. the kinematic variables are the translational acceleration along a first axis perpendicular to gravity and to the platform trajectory, the translational acceleration along a second axis perpendicular to the first axis and to the platform trajectory, and the angular velocities about the first and second axes; and

B. the computation means adjusts the phase reference in accordance with the element of the difference indication corresponding to the translational acceleration along the first axis.

12. An apparatus as defined in claim 1 wherein:

A. the kinematic variables are the translational accelerations in two axes perpendicular to the platform trajectory and rotational velocities about those two axes; and

B. the predicted deviation is the deviation in a state whose elements are the translational velocities in two axes perpendicular to the platform trajectory and the angular velocities about those two axes.

13. An apparatus as defined in claim 1 wherein:

A. the kinematic variables are the translational acceleration along a first axis perpendicular to gravity and to the platform trajectory, the translational acceleration along a second axis perpendicular to the first axis and to the platform trajectory, and the rotational velocities about the first and second axes; and

B. the computation means adjusts the phase reference in accordance with the element of the difference indication that corresponds to the translational acceleration along the first axis.

14. An apparatus as defined in claim 13 wherein the predicted deviation is the deviation in a state whose elements are the translational velocities in two axes perpendicular to the platform trajectory and the angular velocities about those two axes.

15. For guiding a projectile that executes ballistic motion under the influence of gravity and includes a sensor array for sensing, and generating a sensor output representative of, enough physical quantities to determine predetermined kinematic variables if the spin orientation of the platform with respect to gravity is known and further includes moveable control surfaces for affecting the motion of the projectile in accordance with the orientation of the control surface, the method comprising the steps of:

A. establishing a phase reference representing an estimate of the spin phase of the platform with respect to gravity;

B. employing a mathematical model of the platform to calculate a predicted state deviation from an indication of the previous state deviation and to produce a predicted-deviation indication that represents the predicted state deviation;

C. producing from the sensor output, the predicted-deviation indication, and the target-vector indication a difference output representing the difference between (a) the deviation, from the values indicated by the target-vector indication, of the kinematic variables derived from the sensor array in accordance with the phase reference and (b) the deviation, derived from the predicted-deviation indication, of the kinematic variables from the values indicated by the target vector;

D. generating from the predicted-deviation indication and the difference output an estimated-deviation output consisting of the predicted-deviation indication adjusted in accordance with the difference output to represent the new deviation in the state of the platform and using the estimated-deviation output as the indication of the previous state deviation in the next calculation of the predicted state deviation;

E. minimizing any misalignment of the phase reference with the direction of gravity by adjusting the phase reference in accordance with a component of the difference lndication that results from misalignment of the phase reference with the direction of gravity, whereby the phase reference tends to be in alignment with the force of gravity without the need for additional sensors; and

F. moving the control surface so as to control the orientation thereof in accordance with the estimated deviation output.

16. A method as defined in claim 15 wherein the step of producing the difference output includes the steps of:

A. producing correlation values by correlating successive periods of the sensor output with the phase reference;

B. generating a measurement vector by subjecting the correlation values to a transformation that results in a measurement vector having the proper values of the kinematic variables in the absence of sensor noise if the phase reference correctly represents the phase of rotation of the platform with respect to gravity; and

C. generating the difference output by subtracting from the measurement vector the target vector and the deviation in the kinematic variables as derived from the predicted-deviation indication.

17. A method as defined in claim 16 wherein the kinematic variables are different from the state variables in the predicted deviation indication and the step of generating the difference output comprises converting the predicted-deviation indication to the kinematic variables derived therefrom before subtracting the derived kinematic variables from the measurement vector.

18. A method as defined in claim 17 wherein the step of generating the difference output includes producing a first difference by subtracting the target vector from the measurement vector and subtracting from the difference the kinematic variables as derived from the predicted deviation.

19. A method as defined in claim 18 wherein:

A. the kinematic variables are the translational accelerations in two axes perpendicular to the platform trajectory and the rotational velocities about those two axes; and

B. the predicted deviation is the deviation in the state whose elements are the translational velocities in two axes perpendicular to the platform trajectory and the angular velocities about those two axes.

20. A method as defined in claim 17 wherein:

A. the kinematic variables are the translational accelerations in two axes perpendicular to the platform trajectory and the rotational velocities about those two axes; and

B. the predicted deviation is the deviation in the state whose elements are the translational velocities in two axes perpendicular to the platform trajectory and the angular velocities about those two axes.

21. A method as defined in claim 16 wherein:

A. the kinematic variables are the translational acceleration along a first axis perpendicular to gravity and to the platform trajectory, the translational acceleration along a second axis perpendicular to the first axis and to the platform trajectory, and the rotational velocities about the first and second axes; and

B. the step of minimizing phase-reference misalignment includes adjusting the phase reference in accordance with the element of the difference indication that corresponds to the translational acceleration along the first axis.

22. A method as defined in claim 21 wherein the predicted deviation is the deviation in a state whose elements are the translational velocities in two axes perpendicular to the platform trajectory and the angular velocity about those two axes.

23. A method as defined in claim 15 wherein the step of generating an estimated-deviation output comprises the steps of:

A. producing an adjustment vector by converting the difference output to a state deviation and weighting it by a predetermined amount in comparison with the predicted deviation; and

B. adding the adjustment vector to the predicted deviation to produce the estimated-deviation output.

24. A method as defined in claim 23 wherein the step of producing an adjustment vector includes weighting the difference output in a direction favored by modeling errors.

25. A method as defined in claim 24 wherein:

A. the kinematic variables are the translational acceleration along a first axis perpendicular to gravity and to the platform trajectory, the translational acceleration along a second axis perpendicular to the first axis and to the platform trajectory, and the angular velocities about the first and second axes; and

B. the step of minimizing phase-reference misalignment includes adjusting the phase reference in accordance with the element of the difference indication corresponding to the translational acceleration along the first axis.

26. A method as defined in claim 15 wherein:

A. the kinematic variables are the translational accelerations in two axes perpendicular to the platform trajectory and the rotational velocities about those two axes; and

B. the predicted deviation is the deviation in a state whose elements are the translational velocities in two axes perpendicular to the platform trajectory and the angular velocities about those two axes.

27. A method as defined in claim 15 wherein:

A. the kinematic variables are the translational acceleration along a first axis perpendicular to gravity and to the platform trajectory, the translational acceleration along a second axis perpendicular to the first axis and to the platform trajectory, and the angular velocities about the first and second axes; and

B. the step of minimizing phase-reference misalignment includes adjusting the phase reference in accordance with the element of the difference indication corresponding to the translational acceleration along the first axes.

28. A method as defined in claim 27 wherein the predicted deviation is the deviation in a state whose elements are the translation velocities in two axes perpendicular to the platform trajectory and the angular velocities about those two axes.