TWO-AXIS GIMBAL ARRANGEMENT
Assignee
Raytheon
Filed as: RAYTHEON COMPANY, A CORP. OF DE.
Filed
Mar 3, 1982
Granted
Jun 15, 1993
Location
BOXFORD MA US
Abstract
A gyroscopically stabilized optical seeker for use in a cannon-launched projectile is shown to include a gimbal arrangement wherein a two-axis rate gyroscope and associated torque motors are utilized to attain the requisite stabilization however such seeker is oriented with respect to such projectile, the two-axis rate gyroscope being arranged so that the complete optical system, including the detector unit, may be mounted on the inner gimbal.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Aug 11, 1982
Rescinded
Feb 24, 1993
Duration
10 years, 6 months
Inventor
- 1RICHARD A. BECKERLEG
Technology Domains
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Record Details
- Patent number
- US 5219132
- Application
- 00063567
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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