Patent US4006631A successfully refreshed from Google Patents.
US4006631A
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Magnetic heading reference
Assignee: National Aeronautics and Space Administration
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Filing: 1975-10-16
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Granted: 1977-02-08
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Expires: 1995-10-16
Abstract
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.
Inventors
- 👤 Howell D. Garner
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-25 23:45
CPC Classifications
G; G01; G01C; G01C17/00; G01C17/38; G01C17/02; G01C17/28; G01C17/30
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
96 words
Means for correcting the northerly turning error of a magnetic compass on a vehicle comprising: means on said vehicle for generating a signal proportional to V sin φ where V is the vertical component of the earth's magnetic field at the location of the vehicle and φ is the bank angle of the vehicle, and coil means surrounding said compass and receiving said generated signal for generating a force proportional to V sin φ on the needle of said compass in a direction opposite to the force on said needle caused by the northerly turning error.
Claim 2
Dependent Claim
96 words
Means for correcting the northerly turning error of a magnetic compass on a vehicle comprising: means on said vehicle for generating a signal proportional to V sin φ where V is the vertical component of the earth's magnetic field at the location of the vehicle and φ is the bank angle of the vehicle, and coil means surrounding said compass and receiving said generated signal for generating a force proportional to V sin φ on the needle of said compass in a direction opposite to the force on said needle caused by the northerly turning error.
Claim 3
Dependent Claim
39 words
Means for correcting the northerly turning error of a magnetic compass on a vehicle in accordance with claim 1 wherein the sin φ portion of said signal porportional to V sin φ is generated by a vertical free-gyro-mounted transducer.
Claim 4
Dependent Claim
40 words
Means for correcting the northerly turning error of a magnetic compass on a vehicle in accordance with claim 1 wherein the sin φ portion of said signal proportional to V sin φ is generated by a fluidic yaw rate sensor.
Claim 5
Dependent Claim
53 words
Means for correcting the northerly turning error of a magnetic compass on a vehicle in accordance with claim 1 wherein said means for generating a signal proportional to V sin φ includes means for generating a signal proportional to sin φ and means for multiplying the sin φ signal times a constant V.
References Cited (Backward Citations)
US2463245A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1980-02-08 | 1980-08-09 | 1981-02-08 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1984-02-08 | 1984-08-09 | 1985-02-08 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1988-02-08 | 1988-08-09 | 1989-02-08 | $7700.00 | Window Closed / Lapsed |