CONTROL SYSTEM FOR MOVING BODIES
Assignee
SHORT BROTHERS & HARLAND LIMITED
Filed
Mar 15, 1966
Granted
Feb 28, 1995
Location
DOWN IE
Abstract
A missile comprising a first rotatable portion arranged for rotation relative to a second rotatable portion of the missile, the first rotatable portion being adapted to be subjected to a thrust causing it to rotate in one sense during the flight of the body and in the absense of any restraining or opposing forces, and said second rotatable portion being adapted to be subjected to a thrust causing it to rotate in the opposite sense during the flight of the body, steering means on said first rotatable portion for exerting a thrust thereon away from the axis of rotation thereof to produce a steering effect on the missile or body, a free gyroscope mounted in the first rotatable portion and arranged to generate an electrical signal representative of the roll deviation of the first rotatable portion from a predetermined roll attitude in space and electromagnetic braking means responsive to said electrical signal to brake the first rotatable portion against the second rotatable portion to bring said first rotatable portion to said predetermined roll attitude and to hold it in that attitude.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Mar 10, 1982
Rescinded
Apr 15, 1994
Duration
12 years, 1 month
Inventor
- 1ALBERT J. DUNN
Technology Domains
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Record Details
- Patent number
- US 5393012
- Application
- 04536188
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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