Hybrid GPS/inertially aided platform stabilization system

• US 5,948,044 A
• Filed: 05/20/1996
• Issued: 09/07/1999
• Est. Priority Date: 05/20/1996
• Status: Expired due to Fees

• Current Assignee: Xd Semiconductors LLC (Intellectual Ventures LLC)
• Original Assignee: Harris Corporation (L3Harris Technologies, Inc.)
• Inventors: Varley, Robert F., Maney, John J.
• Primary Examiner(s): MARQUIS, LISSI MOJICA
• Application Number:
  US08/650,503
• Time in Patent Office: 1,205 Days
• Field of Search: 701/213, 701/220, 701/221, 701/200
• US Class Current: 701/220
• CPC Class Codes: G01S 19/47 the supplementary measurement being an inertial measurement, e.g. tightly coupled inertial
• CPC Class Codes: G01S 19/54 using carrier phase measurements; using long or short baseline interferometry
• CPC Class Codes: H01Q 1/18 Means for stabilising antennas on an unstable platform
• CPC Class Codes: H01Q 1/3233 particular used as part of a sensor or in a security system, e.g. for automotive radar, navigation systems
• CPC Class Codes: H01Q 3/08 for varying two co-ordinates of the orientation

Abstract

A hybrid system for stabilizing the attitude of an instrument relative to a dynamic platform includes a plurality of (roll, pitch and yaw) inertial rate sensors, whose outputs are sampled at a rate sufficient to provide real time tracking of changes in orientation of the platform, and a global positioning system (GPS) receiver, whose precision platform attitude output is updated periodically, but at a rate less than the rate of change of attitude of the platform. The inertial rate sensors provide effectively continuous motion (e.g., angular rate) data signals representative of three-dimensional changes in attitude (position derivative signals) of the platform. The inertial rate output are integrated to provide output signals representative of the dynamic orientation of the platform. Sequential outputs of the integration-processing circuitry are also coupled to a sample buffer, which is controllably read-out in accordance with the periodic updates from the GPS receiver. The integrated inertial sensor (attitude) data is compared with the GPS update data to generate error signals which are used to adjust the inertial sensor data. By employing a sample buffer in an inertial sensor output integration feedback loop with the GPS receiver, the hybrid system of the present invention avoids what would otherwise be a staleness problem with the data provided by the GPS receiver.

Claims

1. A system for stably positioning the attitude of an instrument relative to a platform upon which the instrument is mounted, said platform having an orientation that is subject to dynamic variations, comprising:

at least one rate of motion sensor attached to said platform, each rate of motion sensor being operative to provide a first, real-time signal representative of rate of change of a respective attitude parameter of said platform;

a platform position sensor which attached to said platform and is operative to generate second signals representative of at least one attitude parameter of said platform; and

a signal processor which is operative to adjust said first signals in accordance with said second signals, and wherein

said platform position sensor comprises a global positioning system (GPS) based platform position sensor, which is operative to periodically generate said second signals at a rate less than that at which said first signals are produced, and wherein said signal processor is operative to generate third signals representative of said attitude parameter of said platform based upon said first signals, and to compare selected ones of said second signals with third signals to derive error signals through which said first signals are adjusted.

2. A system according to claim 1, further including an instrument positioning control mechanism which is operative to control the orientation of said instrument relative to said platform in accordance with said adjusted first signals.

4. A system according to claim 1, wherein said signal processor is operative to adjust a respective first signal in accordance with a most recent update of said second signal.

5. A system according to claim 1, wherein said signal processor includes a storage buffer in which successive third signals are stored, and wherein selected ones of said third signals stored in said storage buffer are accessed in accordance with periodically generated updates of said GPS based platform position sensor, for comparison by said signal processor with said third signals to derive said error signals through which said first signals are adjusted.

6. A system according to claim 5, wherein said signal processor executes a continuous integral of said first signals, producing position signals which are coupled in a feedback path to said storage buffer, so as to make said signal processor smoothly track second signals generated by said GPS based platform position sensor on a long-term basis.

7. A system according to claim 1, wherein said signal processor further includes a correction estimation operator which provides a bias and scale factor adjustment of said first signals in accordance with said error signals.

8. A system according to claim 7, wherein said signal processor is operative to multiply said error signals by a scale factor correction, so as to make motion amplitude of said platform represented by said first signals from said at least one rate of motion sensor agree with an orientation representative second signal generated by said GPS based platform position sensor.

9. A system according to claim 8, wherein said signal processor is operative to multiply said error signals by said scale factor correction in response to said error signals exceeding a prescribed threshold.

10. A system according to claim 7, wherein said signal processor is operative to sum the bias correction adjustment supplied by said correction estimation operator with a first signal generated by a rate of motion sensor.

11. A system according to claim 1, wherein said signal processor includes a coordinate system conversion mechanism which is operative to cause said second signals output by said platform position sensor and said first signals generated by said at least rate of motion sensor to be defined in accordance with a common coordinate system.

3. A system for stably positioning the attitude of an instrument relative to a platform upon which the instrument is mounted, said platform having an orientation that is subject to dynamic variations, comprising:

at least one rate of motion sensor attached to said platform, each rate of motion sensor being operative to provide a first, real-time signal representative of rate of change of a respective attitude parameter of said platform;

a platform position sensor which attached to said platform and is operative to generate second signals representative of at least one attitude parameter of said platform; and

a signal processor which is operative to adjust said first signals in accordance with said second signals, and wherein

said signal processing mechanism includes a sample buffer which stores successive samples of an integral of said first signals, and a buffer read-out control mechanism which is operative to read out a respective output signal sample stored in said sample buffer to be differentially combined with a respective second signal generated by said platform attitude sensor.

12. A method of stably orienting an instrument relative to a platform upon which the instrument is mounted, said platform having an orientation that is subject to dynamic variations, comprising the steps of:

(a) attaching a plurality of rate of motion sensors to said platform, each of said motion sensors being operative to provide a first, real-time signal representative of rate of change of a respectively different attitude parameter of said platform;

(b) providing a platform position sensor which is operative to generate second signals representative of respectively different attitude parameters of said platform;

(c) adjusting said first signals in accordance with said second signals; and

(d) controlling the orientation of said instrument relative to said platform in accordance with said adjusted first signals, and wherein step (c) comprises

(c1) coupling said first signals to an integration operator, which provides output signals representative of the dynamic roll, pitch and yaw orientation of said platform,

(c2) storing said output signals in memory,

(c3) controllably reading out selected ones of said stored output signals from said memory in accordance with periodic updates of said GPS receiver, and

(c4) modifying said first signals in accordance with differences between said selected ones of said output signals and associated ones of said second signals.

14. A method according to claim 12, wherein said platform position sensor is operative to measure the orientation of said platform relative to gravity and geographic north, and wherein said second signals are representative of respectively different instrument gimbal angles of said platform.

24. A method according to claim 12, wherein said rate of motion sensors are operative to generate said first signals representative of rate of roll, pitch and yaw of said platform at a rate sufficient to provide effectively real time tracking of changes in orientation of said platform, and wherein said second signals generated by said global positioning system (GPS) receiver are representative of roll, pitch and yaw orientations of said platform and are updated periodically at a rate less than the rate of change of attitude of the platform.

25. A method according to claim 12, wherein step (c) comprises providing a scale factor correction of said first signals so as to make platform motion amplitude sensed by said rate of motion sensors agree with attitude amplitudes sensed by said GPS receiver.

26. A method according to claim 25, wherein step (c) further comprises providing a bias correction to removes an offset from said first signals generated by said rate of motion sensors as well as cumulative errors in said output signals from said integration operator.

27. A method according to claim 26, wherein step (c) further includes performing a coordinate system conversion operation so as to cause said second signals output by said platform position sensor and said first signals generated by said plurality of rate of motion sensors to be defined in terms of a common coordinate system.

28. A method according to claim 27, wherein step (c) comprises performing body/gimbaled and gimbaled/body coordinate system conversions to account for differences between gimbaled attitude representative second signals generated by said platform position sensor and body rate representative first signals generated by said rate of motion sensors.

29. A method according to claim 28, wherein said platform position sensor comprises a global position system (GPS) receiver.

30. A method according to claim 12, wherein said platform position sensor comprises a global position system (GPS) receiver.

13. A method of stably positioning an instrument relative to a platform upon which the instrument is mounted, said platform having a position and orientation that are subject to dynamic variations, comprising the steps of:

(a) providing at least one inertial rate sensor on said platform, said sensor being operative to generate first signals representative of a rate of change of an attitude parameter of said platform;

(b) providing a global positioning system (GPS) receiver which is operative to generate second signals representative of said attitude parameter of said platform; and

(c) adjusting said first signals in accordance with said second signals, and wherein

said global positioning system (GPS) receiver is operative to periodically generate said second signals at a rate less than that at which said first signals are produced, and wherein step (c) comprises generating third signals representative of said attitude parameter of said platform in accordance with said first signals, and comparing selected ones of said second signals with third signals to derive error signals through which said first signals are corrected.

15. A method according to claim 13, wherein step (c) comprises modifying a respective first signal in accordance with a most recent update of said second signal.

16. A method according to claim 13, wherein step (c) comprises storing successive third signals, and accessing selected ones of said stored third signals in accordance with periodically generated updates of said GPS receiver, for comparison with said third signals to derive said error signals through which said first signals are adjusted.

17. A method according to claim 16, wherein step (c) comprises generating a continuous integral of said first signals to produce said third signals, and coupling third signals in a feedback path to a memory therefor, and selectively reading out third signals stored in said memory in accordance with updates from said GPS receiver.

18. A method according to claim 17, wherein step (c) further comprises reading out a respective third signal stored in said memory to be differentially combined with a respective second signal generated by said GPS receiver.

19. A method according to claim 13, wherein step (c) further comprises providing bias and scale factor adjustment of said first in accordance with said error signals.

20. A method according to claim 19, wherein step (c) comprises multiplying said error signals by a scale factor correction so as to make motion amplitude of said platform represented by said first signals from said at least one inertial rate sensor agree with an orientation representative second signal generated by said GPS receiver.

21. A method according to claim 20, wherein step (c) comprises multiplying said error signals by said scale factor correction in response to said error signals exceeding a prescribed threshold.

22. A method according to claim 18, wherein step (c) comprises summing said bias correction adjustment with said first signal generated by said at least one inertial rate sensor.

23. A method according to claim 13, wherein step (c) further includes performing a coordinate system conversion operation so as to cause said second signals output by said GPS receiver and said first signals generated by said at least one inertial rate sensor to be defined in terms of a common coordinate system.