Geophysical inertial navigation system

• US 6,493,631 B1
• Filed: 05/30/2002
• Issued: 12/10/2002
• Est. Priority Date: 05/31/2001
• Status: Expired due to Term

• Current Assignee: Alan Alexander Burns
• Original Assignee: Mlho, Inc.
• Inventors: Burns, Alan Alexander
• Primary Examiner(s): Camby, Richard M.
• Application Number:
  US10/158,728
• Time in Patent Office: 194 Days
• Field of Search: 701/200, 701/220, 701/221, 701/207, 244/166, 244/171, 731/78.R, 340/988, 340/995
• US Class Current: 701/220
• CPC Class Codes: G01C 17/30 Earth-inductor compasses
• CPC Class Codes: G01C 21/1654 with electromagnetic compass

Abstract

An inertial navigation system employs geophysical (earth'"'"'s magnetic and gravity) field sensors to measure body rotations of an aircraft or other vehicle. In effect, these replace expensive laser ring gyros used in conventional inertial navigation systems. The vector components of the geomagnetic field may be incorporated directly into the state vector describing the vehicle'"'"'s attitude, acceleration, velocity, and position. A predictive filter (e.g. Kalman) operates on measured and predicted geophysical field components and on-board accelerometers. Predicted geophysical field components are obtained from maps and/or models of the earth'"'"'s magnetic and gravity fields.

Claims

1. A system for inertial navigation of a vehicle comprising

a. a means for measuring vector components of a geophysical field;

b. a means for measuring vector components of the acceleration of said vehicle;

c. a means for inertial navigation having as output the geographical position, velocity, and attitude of said vehicle and employing a predictive filter using as inputs;

i. changes in said measured vector geophysical field components;

ii. changes in predicted vector geophysical field components;

iii. said vector components of said vehicle acceleration.

d. a means for employing said geographical position and attitude output of said inertial navigation means to calculate said predicted geophysical field components from descriptive geophysical field data.

2. The system as recited in claim 1 wherein said geophysical field is the earth'"'"'s magnetic field.

3. The system as recited in claim 1 wherein said geophysical field is the earth'"'"'s gravity field.

4. The system as recited in claim 1 wherein said geophysical field is a weighted combination of the earth'"'"'s magnetic field and the earth'"'"'s gravity field.

5. The system as recited in claim 1 wherein said predictive filter is a Kalman filter.

6. The system as recited in claim 1 wherein said geophysical field descriptive data are calculated from one or more models for said geophysical field.

7. The system as recited in claim 1 wherein said geophysical field descriptive data are stored data.

8. The system as recited in claim 1 wherein said geophysical field descriptive data are mapped data.

9. The system as recited in claim 1 wherein said geophysical field descriptive values are a combination of stored data, mapped data, and values calculated from one or more models for said geophysical field.

10. The system as recited in claim 1 wherein the components of said geophysical field are part of said state vector.

11. The system as recited in claim 1 comprising an additional step wherein additional data are employed to augment said navigation process.

12. The system as recited in claim 11 wherein said augmentation is a navigation initialization step.

13. The system as recited in claim 11 wherein said additional data are Global Positioning System navigational data.

14. The system as recited in claim 11 wherein said additional data are a weighted combination of GPS, barometric altimeter, rate of climb, gyroscopic turn (yaw) rate, gyroscopic pitch, gyroscopic roll, gyroscopic yaw, sun or horizon sensors, and radio-navigation device outputs.