Automatic calibration of redundant sensors

• US 5,479,161 A
• Filed: 03/25/1994
• Issued: 12/26/1995
• Est. Priority Date: 03/25/1994
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Weed, Douglas M., Keyes, Charles L.
• Primary Examiner(s): Peng, John K.
• Assistant Examiner(s): Wu, Daniel J.
• Application Number:
  US08/218,485
• Time in Patent Office: 641 Days
• Field of Search: 340/870.01, 340/870.04, 340/945, 340/508, 340/4, 73/1 R, 73/1 E, 364/571.01, 364/571.02, 364/453, 244/175, 244/194, 244/195
• US Class Current: 340/870.04
• CPC Class Codes: G01C 21/188 for accumulated errors, e.g. by coupling inertial systems with absolute positioning systems
• CPC Class Codes: G01C 25/005 initial alignment, calibration or starting-up of inertial devices

Abstract

A system for calibrating the sensors of a redundant sensor system by calculating a first set of error signals based on differences between a combination of the outputs and known values and calculating a second set of error signals based on differences between the parity among preselected sensors and a predetermined value and calculating, from the first and second set of error signals, a plurality of calibration signals to be added to the output of the individual sensors which are in error so as to correct their outputs.

Claims

1. Calibration apparatus for use with redundant condition responsive sensors having outputs indicative of the conditions sensed which outputs may contain errors produced by individual sensors comprising:

first computer means connected to receive the outputs of the sensors and to produce outputs indicative of desired conditions derived from the conditions sensed by the sensors;

second computer means connected to receive the outputs from the first computer means, to compare the outputs from the first computer means with known values for the desired conditions and to produce a first plurality of signals partially indicative of any errors from the sensors;

third computer means connected to receive the outputs of the sensors and to produce parity signals indicative of any difference between preselected combinations of weighted outputs of the sensors with a predetermined value;

fourth computer means connected to receive the parity signals and to produce a second plurality of signals partially indicative of any errors from the sensors;

mapper means connected to receive the first and second plurality of signals from the second and fourth computer means and to produce error correcting signals indicative of the errors produced by individual sensors; and

feedback means connecting the error correcting signals to the outputs of the sensors to modify the outputs of any sensors that are in error so as to calibrate them.

2. Apparatus according to claim 1 wherein the feedback means further includes summing means for adding the error correcting signals to the signals from the sensors.

3. Apparatus according to claim 1 wherein the sensors include at least four gyros and the desired conditions from the first computer means comprise position.

4. Apparatus according to claim 3 wherein the position condition is at least longitude and latitude.

5. Apparatus according to claim 1 wherein the sensors include at least four accelerometers and the desired conditions comprise velocity.

6. Apparatus according to claim 5 wherein the velocity condition is at least velocity in north and east directions.

7. Apparatus according to claim 1 wherein the sensors include six gyros and six accelerometers and the desired conditions from the first computer means are at least longitude, latitude, velocity in the north direction and velocity in the east direction.

8. Apparatus according to claim 7 wherein the second computer means is also connected to receive inputs indicative of actual longitude, latitude, velocity in the north direction and velocity in the east direction to compare them with the outputs from the first computer means.

9. Apparatus according to claim 7 wherein the desired conditions from the first computer means are longitude, latitude, altitude, velocity in the north direction, velocity in the east direction and velocity in the verticle direction.

10. Apparatus according to claim 7 wherein the third computer means operates to combine the outputs of the six gyro in different ways to produce three parity signals and to combine the output of the six accelerometers to produce three more parity signals.

11. The method of calibrating a redundant plurality of sensors each producing an output signal indicative of a condition which signal may contain an error, comprising the steps of:

A. combining the outputs of the sensors to produce a first set of combined signals indicative of predetermined conditions;

B. comparing the first set of combined signals with a second set of signals indicative of the known values of the predetermined conditions and producing a first plurality of error signals indicative of any difference;

C. combining the outputs of the sensors to produce a second set of combined signals inductive of parity conditions;

D. producing a second plurality of error signals from the second set of combined signals indicative of any difference between the second set of combined signals and desired values;

E. computing form the first and second plurality of error signals a plurality calibration signals indicative of any errors produced by the plurality of sensors; and

F. combining the calibration signals with the output signals of the sensors to effect calibration thereof.

12. The method of claim 11 wherein the sensors are more than three gyros and the first set of combined signals comprises a signal indicative of position.

13. The method of claim 11 wherein the sensors are more than three gyros and more than three accelerometers and the first set of combined signals comprises signals indicative of position and velocity.

14. The method of claim 11 wherein the sensors are at least six gyros and six accelerometers of an aircraft and the first set of combined signals comprises a first group of signals indicative of the position of the aircraft in at least two directions, and a second group of signals indicative of the velocity of the aircraft in the two directions.

15. The method of claim 14 wherein the two directions are latitude and longitude.

16. The method of claim 11 wherein the sensors are at least six gyros and six accelerometers of an aircraft and the first set of combined signals comprises a first group of signals indicative of the position of the aircraft in three directions, and a second group of signals indicative of the velocity of the aircraft in the three directions.

17. Apparatus according to claim 16 wherein the first group of signals is indicative of latitude, longitude and altitude.