Patent US3351471A successfully refreshed from Google Patents.
Patent US4646990A successfully refreshed from Google Patents.
US4646990A
Expired / Lapsed
US
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Magnetic roll sensor calibrator
Assignee: Lockheed Martin Corp
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Filing: 1986-02-18
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Granted: 1987-03-03
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Expires: 2006-02-18
Abstract
Abstract A coil (21) mounted inside a spinning guided object (20) has an electrical current (i) induced therewithin by means of interaction with the earth's magnetic field (B). A similar coil (22) mounted on the launch platform spins at the same rate (W) as the object's coil (21), although these two coils (22, 21) are not necessarily in phase. Apparatus (35) associated with the launch platform generates a constant phase signal (P) having amplitude and sign representing the phase difference between the signal generated by the launch platform's coil (22) and the vertical direction. This phase information (P) is used to correct the guidance commands sent from the launch platform to the guided object (20), or, alternatively, is fed directly to the guided object (20) for correction by said object's on-board computer. A hold fire indicator (33) is provided to inform the operator when the output from the launch platform's coil (22) is above or below a predetermined level sufficient for adequate roll angle compensation.
Inventors
- 👤 William C. Cleveland, Jr.
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 13:39
CPC Classifications
F; F41; F41G; F41G7/00; F41G7/20; F41G7/30; F41G7/301; F41G7/305
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
159 words
Apparatus for determining the roll angle of a spinning guided object that has been launched from a launch platform, said apparatus comprising: on board the guided object, a first coil which has an electrical voltage induced therewithin by the earth's magnetic field as the guided object spins along its trajectory; mounted on the launch platform, a second coil which spins about an axis at the same rate as the first coil, and thereby has an electrical voltage induced therewithin by the earth's magnetic field; mounted on the launch platform, means for correlating the voltage within the second coil with the vertical direction, said correlating means having inputs coupled to the second coil and to a vertical reference, respectively; and means for conveying to the guided object the phase relationship between the voltage within the second coil and the vertical direction, said conveying means having inputs coupled to the second coil and to an output of the correlating means, respectively.
Claim 2
Dependent Claim
159 words
Apparatus for determining the roll angle of a spinning guided object that has been launched from a launch platform, said apparatus comprising: on board the guided object, a first coil which has an electrical voltage induced therewithin by the earth's magnetic field as the guided object spins along its trajectory; mounted on the launch platform, a second coil which spins about an axis at the same rate as the first coil, and thereby has an electrical voltage induced therewithin by the earth's magnetic field; mounted on the launch platform, means for correlating the voltage within the second coil with the vertical direction, said correlating means having inputs coupled to the second coil and to a vertical reference, respectively; and means for conveying to the guided object the phase relationship between the voltage within the second coil and the vertical direction, said conveying means having inputs coupled to the second coil and to an output of the correlating means, respectively.
Claim 3
Dependent Claim
33 words
Apparatus of claim 1 wherein the phase relationship between the voltage within the second coil and the vertical direction is incorporated into guidance commands conveyed to the guided object from the launch platform.
Claim 4
Dependent Claim
53 words
Apparatus of claim 1 wherein the phase relationship between the voltage within the second coil and the vertical direction is sent directly to the guided object from the launch platform, said apparatus further comprising means on board the guided object for correcting the voltage measured at the first coil with said phase relationship.
Claim 5
Dependent Claim
81 words
Apparatus of claim 1 wherein the conveying means comprises a phase comparator having first and second inputs and an output, wherein: the first input is coupled to a signal representing the voltage induced in the second coil; the second input is coupled to a signal which emanates from the correlating means and periodically indicates when the second coil is in a vertical orientation; and the output conveys a signal representing the phase between the voltage within the second coil and vertical.
Claim 6
Dependent Claim
76 words
Apparatus of claim 1 wherein the correlating means comprises: coupled to the spinning second coil, means for generating a first voltage proportional to the angle of rotation of the second coil about its axis of rotation; means for generating a second voltage representing angular deviations from the vertical direction; and means for subtracting the second voltage from the first voltage to produce a signal which periodically indicates when the second coil is in a vertical orientation.
Claim 7
Dependent Claim
82 words
Apparatus of claim 1 further comprising means for determining when the voltage in the second coil is too weak to produce a reliable roll angle indication, said determining means comprising a comparator having first and second inputs and an output, wherein: the first input is coupled to a signal representing voltage within the second coil; the second input is coupled to a predetermined reference voltage; and the output conveys a signal indicating whether the roll angle indication is deemed to be reliable.
Claim 8
Dependent Claim
33 words
Apparatus of claim 1 wherein, during at least initial portions of the object's flight, the axis of rotation of the first coil is parallel to the axis of rotation of the second coil.
Claim 9
Dependent Claim
18 words
Apparatus of claim 1 wherein the first coil lies in a plane containing the guided object's spin axis.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1990-03-02 | 1990-09-01 | 1991-03-03 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-03-02 | 1994-09-01 | 1995-03-03 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-03-02 | 1998-09-01 | 1999-03-03 | $7700.00 | Window Closed / Lapsed |