Fault tolerant inertial reference system

• US 5,719,764 A
• Filed: 07/19/1995
• Issued: 02/17/1998
• Est. Priority Date: 07/19/1995
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: McClary, Charles R.
• Primary Examiner(s): Elmore, Reba I.
• Assistant Examiner(s): MARC, MCDIEUNEL
• Application Number:
  US08/504,106
• Time in Patent Office: 944 Days
• Field of Search: 364/184, 364/183, 364/190, 364/459, 364/943.9, 364/944.8, 364/945.4, 364/945.8, 364/946.1, 342/352
• US Class Current: 700/79
• CPC Class Codes: G01C 21/165 combined with non-inertial navigation instruments
• CPC Class Codes: G05B 9/03 with multiple-channel loop, i.e. redundant control systems
• CPC Class Codes: G05D 1/0077 using redundant signals or controls

Abstract

A fault tolerant inertial reference system employs two independent inertial reference units each having its own inertial sensor array with redundant output information. Each inertial reference unit includes an independent source of position and velocity information through employment of a satellite positioning system. In turn, a high-speed error estimator processes inertial sensor output data from a local inertial sensor array with inertial sensor output data from another external inertial sensor array for determining high-level errors, and a low-speed error estimator processes output data from the local inertial sensor array with the velocity and position information separately obtained from the satellite positioning system for determining low-level errors. In turn these high and low-level errors are processed to determine a fault-free inertial sensor configuration for subsequently determining reliable fault tolerant inertial reference data obtainable with a minimum set of inertial sensors.

Claims

1. A fault tolerant inertial reference system comprising:

a first inertial reference unit including,

a first array of at least four inertial sensors mounted along skewed axes to a support frame for providing a first array of inertial sensor outputs,

a first satellite positioning system position estimator for obtaining first positional information related to said support frame,

means for determining first low-speed inertial sensor error estimates as a function of said first array of inertial sensor outputs, said first positional information, and first fault-free inertial sensor configuration information,

means for determining first high-speed inertial sensor error estimates as a function of said first array of inertial sensor outputs, a second array of inertial sensor outputs from a second array of at least four inertial sensors mounted along skewed axes to said support frame, independent of said first array of inertial sensors, and said first fault-free inertial sensor configuration information,

first fault isolation and reconfiguration means, responsive to said first low-speed error estimates and said first high-speed error estimates, for determining said first fault-free inertial sensor configuration information indicative of any faulty inertial sensors of said first inertial sensor array, and

first inertial reference processor responsive to said first fault-free inertial sensor configuration and said first array of inertial sensor outputs for providing first fault tolerant inertial reference information derived from those ones of said first array of inertial sensor being fault-free; and

a second inertial reference unit including,

said second array of inertial sensors for providing said second array of inertial sensor outputs,

a second satellite positioning system position estimator for obtaining second positional information related to said support frame,

means for determining second low-speed inertial sensor error estimates as a function of said second array of inertial sensor outputs, said second positional information obtained from said second satellite positioning system position estimator, and second fault-free inertial sensor configuration information,

means for determining second high-speed inertial sensor error estimates as a function of said first array of inertial sensor outputs, said second array of inertial sensor outputs, and said second fault-free inertial sensor configuration information,

second fault isolation and reconfiguration means, responsive to said second low-speed error estimates and said second high-speed error estimates, for determining said second fault-free inertial sensor configuration information indicative of any faulty inertial sensors of said second inertial sensor array, and

second inertial reference processor responsive to said second fault-free inertial sensor configuration and said second array of inertial sensor outputs for providing second fault tolerant inertial reference information derived from those ones of said second array of inertial sensors being fault-free.

2. The fault tolerant inertial reference system of claim 1 wherein:

said first inertial reference unit includes a fault detection means responsive to said first array of inertial sensor outputs for providing a first fault signal indicative of the existence of a faulty one of said first array of inertial sensors, and where in said first fault isolation and reconfiguration means is responsive thereto, and,

said second inertial reference unit includes a fault detection means responsive to said second array of inertial sensor outputs for providing a second fault signal indicative of the existence of a faulty one of said second array of inertial sensors, and wherein said second fault isolation and reconfiguration means is responsive thereto.

3. The fault tolerant inertial reference system of claim 1 wherein said first and second positional information includes position and velocity information related to said support frame.

4. The fault tolerant inertial reference system of claim 1 wherein said first and second fault isolation and reconfiguration means is operative for comparing said first and second low-speed and said first and second high-speed inertial sensor error estimates, respectively, to selected maximum values.

5. The fault tolerant inertial reference system of claim 1 wherein said means for obtaining said first low-speed inertial sensor error estimates includes a Kalman filter for operating on said first array of inertial sensor outputs and said first positional information for deriving said low-speed inertial sensor error estimates, and said means for obtaining said second low-speed inertial sensor error estimates includes a Kalman filter for operating on said second array of inertial sensor outputs and said second positional information for deriving said low-speed inertial error estimates.

6. The fault tolerant inertial reference system of claim 5 wherein said Kalman filter is a narrow bandwidth Kalman filter.

7. The fault tolerant inertial reference system of claim 1 wherein said means for obtaining said first high-speed inertial sensor error estimates includes a Kalman filter for operating on said first and second array of inertial sensor outputs for deriving said high-speed inertial sensor error estimates, and said means for obtaining said second high-speed inertial sensor error estimates includes a Kalman filter for operating on said first and second array of inertial sensor outputs for deriving said high-speed inertial sensor error estimates.

8. The fault tolerant inertial reference system of claim 5 wherein said Kalman filter is a wide bandwidth Kalman filter.

9. The fault tolerant inertial reference system of claim 1 where each of said means for determing said first and second high-speed inertial sensor error estimates includes means for determing the spatial relationship between said first and second arrays of inertial sensors as function of said first and second array of inertial sensor outputs, and wherein each of said first and second high-speed error estimates is a function of said spatial relationship.

10. The fault tolerant inertial reference system of claim 1 wherein said first low speed inertial sensor error estimates is a function of the differences between said first positional information and like-kind positional information derived from said first array of inertial sensor outputs, and said second low speed inertial sensor error estimates is a function of the differences between said second positional information and like-kind positional information derived from said second array of inertial sensor outputs.