US4993274A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Gyroscope system
Assignee: BAE Systems PLC
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Filing: 1989-02-03
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Granted: 1991-02-19
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Expires: 2009-02-03
Abstract
Abstract A gyroscope system comprises a dual-axis rate gyroscope (1) including angle pick-offs and rotor torque applying device (5), and a control circuit (3) arranged to supply a control signal to the rotor torque applying device (5) in accordance with the output angle sensed by the angle pick-offs. The system further comprises an angular acceleration sensor (2) which is independent of the dual-axis rate gyroscope and is arranged to output a signal to the control circuit (3). The signal modifies in accordance with the sensed angular acceleration the control signal supplied to the torque applying device (5). Preferably the angular acceleration sensor (2) forms part of a guidance system independent of the dual-axis rate gyroscope (1).
Inventors
- 👤 Geoffrey Downton
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-03 05:35
CPC Classifications
G; G01; G01C; G01C19/00; G01C19/02; G01C19/04; G01C19/30; G01C19/42; Y; Y10; Y10T; Y10T74/00; Y10T74/12; Y10T74/1229; Y10T74/1232; Y10T74/125; Y10T74/1261; Y10T74/1279
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
145 words
A dual-axis rate gyroscope system comprising: a support platform; a rotor mounted for rotation relative to the support platform and for angular displacement relative thereto, said rotor having a rate of rotation; transducer means, coupled to the rotor, for forming a first electrical signal representative of said angular displacement of the rotor relative to the platform; torque applying means, coupled to the rotor and responsive to a torque signal, for precessing said rotor and for cancelling said angular displacement of said rotor for a range of values independent of said rate of rotation; angular acceleration sensing means, supported by said platform, for forming a second electrical signal representative of angular acceleration of the platform; and control loop means, connected to said transducer means, said angular acceleration sensing means and said torque applying means, for combining said first and second electrical signals forming said torque signal.
Claim 2
Dependent Claim
145 words
A dual-axis rate gyroscope system comprising: a support platform; a rotor mounted for rotation relative to the support platform and for angular displacement relative thereto, said rotor having a rate of rotation; transducer means, coupled to the rotor, for forming a first electrical signal representative of said angular displacement of the rotor relative to the platform; torque applying means, coupled to the rotor and responsive to a torque signal, for precessing said rotor and for cancelling said angular displacement of said rotor for a range of values independent of said rate of rotation; angular acceleration sensing means, supported by said platform, for forming a second electrical signal representative of angular acceleration of the platform; and control loop means, connected to said transducer means, said angular acceleration sensing means and said torque applying means, for combining said first and second electrical signals forming said torque signal.
Claim 3
Dependent Claim
42 words
The system of claim 1, wherein said angular acceleration sensing means comprises a rate gyroscope and processing means, operatively connected to said rate gyroscope, for processing a signal from said rate gyroscope thereby producing said signal dependent on said sensed angular acceleration.
Claim 4
Dependent Claim
23 words
The system of claim 2, wherein said angular acceleration sensing means comprises part of a guidance system independent of said dual-axis rate gyroscope.
Claim 5
Dependent Claim
44 words
The system of claim 1, wherein said angular acceleration sensing means comprises two linear accelerometers and processing means, operatively connected to said two linear accelerometers, for processing, a signal from said two linear accelerometers thereby producing said output dependent on said sensed angular acceleration.
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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) | 1994-02-18 | 1994-08-20 | 1995-02-19 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1998-02-18 | 1998-08-20 | 1999-02-19 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2002-02-18 | 2002-08-20 | 2003-02-19 | $7700.00 | Window Closed / Lapsed |