Gravity aided inertial navigation system

• US 5,339,684 A
• Filed: 12/10/1991
• Issued: 08/23/1994
• Est. Priority Date: 12/10/1991
• Status: Expired due to Term

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Textron Inc
• Inventors: Dosch, Daniel E., Jircitano, Albert
• Primary Examiner(s): Gregory, Bernarr E.
• Application Number:
  US07/805,544
• Time in Patent Office: 987 Days
• Field of Search: 73/178 R, 364/453, 364/454
• US Class Current: 73/178.00R
• CPC Class Codes: G01C 21/166 Mechanical, construction or arrangement details of inertial navigation systems
• CPC Class Codes: G01C 21/185 for gravity
• CPC Class Codes: G01C 21/188 for accumulated errors, e.g. by coupling inertial systems with absolute positioning systems

Abstract

An autonomous covert Inertial Navigation System uniquely suited for underwater applications wherein Schuler and siderial errors are bounded without external navigation aids or active instrumentation of ground speed is achieved by integrating a conventional Inertial Navigation System with a gravity gradiometer capable of measuring gravity field components independently of platform accelerations.

Claims

1. A navigation system, comprising:

a gravity gradiometer means;

a three axis inertial position determining means including a vertical accelerometer means;

a vertical displacement sensor; and

an optimal filter means for integrating electronic outputs from said gravity gradiometer means, said three axis inertial position determining means and said vertical displacement sensor.

2. A navigation system as defined in claim 1 wherein said gravity gradiometer means measures less than every element of the complete local gravity gradient tensor and produces estimates of the local gravity field.

3. A navigation system as defined in claim 1 wherein said gravity gradiometer means comprises:

a plurality of accelerometers mounted on a rotatable support mounting means;

means for rotating said rotatable support mounting means; and

a housing for said means for rotating and said rotatable support mounting means supported by a stabilized platform.

4. A navigation system as defined in claim 3 wherein said gravity gradiometer means comprises:

a shake accelerometer oriented along the axis of said rotatable support mounting means and mechanically coupled thereto;

a shake actuator mechanically coupled to said shake accelerometer; and

spring bias means for supporting said shake actuator and said shake accelerometer within said housing.

5. A navigation system as defined in claim 3 wherein said plurality of accelerometers comprises four accelerometer.

6. A navigation system as defined in claim 3 wherein said plurality of accelerometers are mounted tangentially and equally spaced apart radially on said rotatable support mounting means.

7. A navigation system as defined in claim 1 wherein said gravity gradiometer means comprises one to three rotating gravity gradiometers.

8. A navigation system as defined in claim 1 adapted to function as a gravity survey system.

9. A navigation system as defined in claim 1 wherein said gravity gradiometer means measures every element of the complete local gravity gradient tensor and produces estimates of the local gravity field.

10. A navigation system, comprising:

a gradiometer means comprising from one to three gradiometers each comprising four rotating accelerometers mounted tangentially at cardinal points on a rotating means;

a three axis inertial position determining means including a gravimeter grade vertical accelerometer;

a depth sensor; and

an optimal filter means for integrating outputs from said gradiometer means;

said three axis inertial position determining means and said depth sensor.