Alignment error calibrator and compensator

• US 4,488,249 A
• Filed: 02/04/1982
• Issued: 12/11/1984
• Est. Priority Date: 02/04/1982
• Status: Expired due to Term

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Martin Marietta Corporation
• Inventors: Baker, Edward B.
• Primary Examiner(s): Smith, Jerry
• Assistant Examiner(s): Huang, Karl
• Application Number:
  US06/345,892
• Time in Patent Office: 1,041 Days
• Field of Search: 364/571, 364/516, 364/453, 364/454, 364/559, 73/1 E, 358/125
• US Class Current: 702/92
• CPC Class Codes: F41G 3/326 for checking the angle between the axis of the gun sighting device and an auxiliary measuring device F41G3/323 takes precedence
• CPC Class Codes: F41G 5/18 Tracking systems for guns on aircraft

Abstract

In an airborne target acquisition and tracking system having a stabilization axis and an optical axis in which a slight mechanical misalignment is present, an apparatus and method for electronically compensating for such misalignment. A roll rate sensing circuit in the system produces a signal when the aircraft rolls. A yaw scaling factor circuit and a pitch scaling factor circuit operate on the roll rate signal and apply scaled versions thereof to the yaw rate servo subsystem and the pitch rate servo subsystem respectively to cancel a yaw rate error signal and a pitch rate error signal produced by the mechanical misalignment. The required scale factors are automatically adjusted by use of a calibrate mode by microprocessors that calculate the ratio of yaw and pitch error signals, generated by artifically rolling the system, to the roll rate signal also generated. The measured ratios are stored in non-volatile memories functioning when the system is in the operate mode. Alternatively, the system control computer may be programmed to provide the above noted calibration and compensation functions.

Claims

1. In an airborne optical target acquisition and tracking system having an optical subsystem disposed on a stabilized platform, said platform controlled by an elevation drive, an azimuth drive, a roll rate sensing circuit, a pitch rate servo, and a yaw rate servo, apparatus for calibrating and compensating the system for misalignment between the stabilization axis of said platform and the axis of said optical subsystem comprising:

(a) scaling means connected to said roll rate sensing circuit to receive roll rate signals therefrom, and having pitch error signal output connected to said yaw rate servo, and yaw error signal output connected to said pitch rate servo, said scaling means for producing an error singal at said pitch error signal output proportional to the yaw component of said misalignment, and an error signal at said yaw error signal output proportional to the pitch component of said misalignment; and

(b) calibration means including

(i) low frequency oscillator means connected to said azimuth drive for moving said platform in yaw, thereby producing a roll rate proportional to said misalignment and a roll rate signal from said roll rate sensing circuit for calibration of said system,

(ii) first adjustment means connected to said scaling means for adjusting said pitch error signal output due to said low frequency oscillator to compensate for an azimuthal component of said misalignment, and

(iii) second adjustment means connected to said scaling means for adjusting said yaw error signal output due to said low frequency oscillator to compensate for an elevational component of said misalignment.

2. The apparatus as defined in claim 1 in which said first adjustment means comprises a pitch voltage divider having its input connected to said roll rate sensing circuit and having a first adjustable output, said second adjustment means comprises a yaw voltage divider having its input connected to said roll rate sensing circuit and having a second adjustable output, and said scaling means includes a yaw amplifier having its input connected to said second adjustable output and an output connected to the input of said yaw rate servo, and a pitch amplifier having its input connected to said first adjustable output and an output connected to the input of said pitch rate servo.

3. The apparatus defined in claim 2 in which said first and second adjustment means include pitch tracking and yaw tracking target acquisition display means for indicating when said first and second adjustment means are correctly adjusted.

4. The apparatus as defined in claim 1 in which said scaling means comprises:

pitch scale factor memory means having an input connected to said roll rate sensing circuit, a dc pitch error signal input, an output connected to said yaw rate servo, and a first switch having a calibrate and an operate position;

yaw scale factor memory means having an input connected to said roll rate sensing circuit, a dc yaw error signal input, an output connected to said pitch rate servo, and a second switch having a calibrate and an operate position;

a pitch rate servo tracker output for producing a pitch error output signal responsive to said low frequency oscillator means, said pitch error output signal being proportional to the yaw component of said misalignment;

a yaw rate servo tracking output for producing a yaw rate error output signal responsive to said low frequency oscillator means, said yaw error output signal being proportional to the pitch component of said misalignment;

a pitch rate error output signal magnitude measuring means connected to said yaw rate servo tracking error output via a third switch having a calibrate and an operate position, for producing a dc pitch error signal, said dc pitch error signal being communicated to said dc pitch error signal input of said yaw scale factor memory means;

a yaw rate error output signal magnitude measuring means connected to said pitch rate servo tracking error output via a fourth switch having a calibrate and an operate position, for producing a dc yaw error signal, said dc yaw error signal being communicated to said dc yaw error signal input of said pitch scale factor memory means;

said yaw scale factor memory means including first calculating means for calculating a first ratio of the peak value of signals from said roll rate sensing circuit to said dc yaw error signal and first non-volatile memory for storing said first ratio; and

said pitch scale factor memory means including second calculating means for calculating a second ratio of the peak value of signals from said roll rate sensing circuit to said dc pitch error signal and second non-volatile memory for storing said second ratio.

5. The apparatus as defined in claim 4 in which each of said pitch and yaw rate error magnitude measuring means respectively comprises:

a correlator having an input from said low frequency oscillator and from a respective pitch or yaw tracking error output;

a low pass filter connected to receive the output of said correlator, thereby producing at its output a slowly varying error signal; and

a sample and hold circuit connected to receive said varying error signal for producing a peak dc error signal.

6. The apparatus as defined in claim 5 in which said pitch and yaw scale factor memories each comprise:

a first analog-to-digital converter connected to the output of said roll rate sensing circuit;

a second analog-to-digital converter connected to the output of said sample and hold circuit;

microprocessor means having a calibrate/operate switch connected thereto and a non-volatile memory associated therewith, said microprocessor means connected to the outputs of said first and second analog-to-digital converters;

said microprocessor means, when said switch is in its calibrate position, for calculating digitally the magnitude of a roll rate signal received from said first analog-to-digital converter and calculating its ratio to the amplitude of the sample and hold circuit output from said second analog-to-digital converter, said microprocessor means storing said ratio in said non-volatile memory means whereby such value remains stored in said memory means when said switch is switched to its operate position, said microprocessor means thereafter changing the amplitude of incoming roll rate signals by said stored ratio; and

digital-to-analog converter means connected to receive such scaled roll rate signals from said microprocessor means for adding to respective pitch and yaw rate commands to said servos when said switch is in its operate position.

7. An airborne optical target acquisition and tracking system having an optical system disposed on a platform stabilized in pitch and yaw in which the stabilization axis is slightly misaligned with respect to the optical system axis comprising:

a pitch rate servo system for controlling said platform in pitch having a pitch summing input;

a yaw rate servo system for controlling said platform in yaw having a yaw summing input;

a roll rate sensing circuit for producing a roll rate output signal;

a command computer connected to said summary inputs of said pitch and yaw rate servo systems for controlling the position of said optical system axis with respect to a target;

a first scaling factor circuit connected to receive said roll rate output signal from said roll rate sensing circuit for producing a yaw compensating signal at said yaw summing input proportional to the effect of said misalignment on said platform in pitch; and

a second scaling factor circuit connected to receive said roll rate output signal from said roll rate sensing circuit for producing a pitch compensating signal at said pitch summing input proportional to the effect of said misalignment on said platform in yaw.

8. In an airborne optical target acquisition and tracking system having pitch and yaw rate servo subsystems for stabilizing a platform supporting an optical subsystem, and a computer for controlling the pitch and yaw servo subsystems, a method for calibrating the system to compensate for mechanical misalignment between the optical axis of the optical system and the stabilization axis of the platform comprising the steps of:

acquiring and tracking a fixed optical target with the system;

producing a rolling motion of the system so as to produce an apparent motion of the target with respect to the stabilization axis;

producing a roll rate signal from such rolling motion;

modifying the amplitude of the roll rate signal by a first adjustable gain amplifier;

summing the first modified amplitude roll rate signal with pitch computer commands to the pitch rate servo subsystem;

modifying the amplitude of the roll rate signal by a second adjustable gain amplifier;

summing the second modified amplitude roll rate signal with computer command signals to the yaw rate servo subsystem; and

adjusting the first and second adjustable gain amplifiers until the apparent motion of the target with respect to the stabilization axis is reduced essentially to zero.

9. The method defined in claim 8 in which the adjusting step includes the steps of:

observing apparent target motion on a system display; and

performing the adjustment until the target remains at the center of the display.

10. The method defined in claim 8 in which the adjusting step includes the steps of:

measuring the target tracking voltages in the system; and

performing the adjustment until the target tracking voltages are essentially zero.

11. In an airborne optical target acquisition and tracking system having a four gimballed, gyro stabilized platform for supporting an optical subsystem, a roll rate sensing circuit, a pitch rate servo, a yaw rate servo, a non-volatile pitch memory connected to the roll rate sensing circuit output, a non-volatile yaw memory connected to the roll rate sensing circuit output, and a computer for controlling the platform for tracking of targets, a method for calibrating and compensating the system for misalignment between the stabilization axis of the platform and the axis of the optical subsystem comprising the steps of:

A. disposing a fixed optical target at an acute angle in pitch from the horizontal;

B. acquiring the fixed optical target;

C. applying a low frequency sinusoidal signal to the yaw rate servo to thereby produce

(a) a rolling motion of the platform proportional to the mechanical misalignment between the stabilization axis and the optical axis,

(b) a pitch tracking error signal from the computer,

(c) a yaw tracking error signal from the computer, and

(d) a roll rate signal from the roll rate sensing circuit;

D. correlating the low frequency sinusoidal signal with the pitch tracking error signal;

E. correlating the low frequency sinusoidal signal with the yaw tracking error signal;

F. producing a pitch tracking error dc signal amplitude from the pitch correlation step;

G. producing a yaw tracking error dc signal amplitude from the yaw correlation step;

H. calculating the ratio between the amplitude of the roll rate signal and the pitch tracking error dc amplitude signal;

I. storing the pitch tracking error ratio in a non-volatile memory;

J. calculating the ratio between the amplitude of the roll rate signal and the yaw tracking error dc amplitude signal;

K. storing the yaw tracking error ratio in a non-volatile memory;

L. disconnecting the sinusoidal signal from the yaw rate servo;

M. producing a yaw rate compensation signal by scaling an output from the roll rate sensing circuit with the stored yaw tracking error ratio, and summing the yaw rate compensation signal with the input to the pitch rate servo; and

N. producing a pitch rate compensation signal by scaling an output from the roll rate sensing circuit with the stored pitch tracking error ratio, andsumming the pitch rate compensation signal with the input to the yaw rate servo.

12. The method as defined in claim 11 which further comprises the steps of:

O. placing the system in an operate mode;

P. scaling the roll rate signal when present by the stored pitch tracking error ratio to produce the first scaled roll rate signal;

Q. summing the first scaled roll rate signal with computer command signals to the yaw rate servo;

R. scaling the roll rate signal when present by the stored yaw tracking error ratio to produce the second scaled roll rate signal; and

S. summing the second scaled roll rate signal with computer command signals to the pitch rate servo.