Magnetic heading reference

• US 3,943,763 A
• Filed: 12/11/1974
• Issued: 03/16/1976
• Est. Priority Date: 12/11/1974
• Status: Expired due to Term

• Current Assignee: The United States of America As Represented By The United States National Aeronautics and Space Administration Office of General Counsel-Code GP
• Original Assignee: United States of America As Represented By The United States National Aeronautics and Space Administration Office of General Counsel-Code GP
• Inventors: Garner, Howell D.
• Primary Examiner(s): Woodiel, Donald O.
• Application Number:
  US05/531,647
• Time in Patent Office: 461 Days
• Field of Search: 33/356, 33/357, 33/358, 73/178 R, 73/178 T
• US Class Current: 73/178.00R
• CPC Class Codes: G01C 17/30 Earth-inductor compasses
• CPC Class Codes: G01C 17/38 Testing, calibrating, or compensating of compasses

Abstract

This invention employs a magnetometer as a magnetic heading reference for a vehicle such as a small aircraft. The magnetometer is mounted on a directional dial in the aircraft in the vicinity of the pilot such that it is free to turn with the dial about the yaw axis of the aircraft. The invention includes a circuit for generating a signal proportional to the northerly turning error produced in the magnetometer due to the vertical component of the earth'"'"'s magnetic field. This generated signal is then subtracted from the output of the magnetometer to compensate for the northerly turning error.

Claims

1. A vehicle heading reference comprising:

a directional dial mounted on said vehicle so that it can be turned about an axis parallel to the yaw axis of said vehicle;

a magnetometer mounted on said directional dial such that its longitudinal axis coincides with said axis parallel to the yaw axis of said vehicle so that it is rotatable with said directional dial wherein the magnetometer produces an output signal related to the difference between the directional dial setting and the actual heading of said vehicle;

means on said vehicle for generating a signal related to the northerly turning error; and

means for subtracting said signal related to the northerly turning error from said output signal produced by said magnetometer whereby the resulting signal is an output signal corrected for the northerly turning error.

2. A vehicle heading reference according to claim 1 wherein said means for generating a signal related to the northerly turning error is means for generating a signal related to

3. A vehicle heading reference according to claim 2 wherein the sin φ

portion of said signal related to K sin φ

cos H is generated by a vertical free-gyro-mounted transducer.

4. A vehicle heading reference according to claim 2 wherein the sin φ

portion of said signal related to K sin φ

cos H is generated by a fluidic yaw rate sensor.

5. A vehicle heading reference according to claim 2 wherein the cos H portion of said signal related to K sin φ

cos H is generated by coils that surround said magnetometer and fixed to said vehicle so that the direction of the magnetic field generated by the coils is parallel to the pitch axis of the vehicle.

6. A vehicle heading reference according to claim 2 wherein the cos H portion of said signal related to K sin φ

cos H is generated by a scotch yoke fixed to said magnetometer.