Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1992-03-23
1993-07-13
Eldred, J. Woodrow
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
244 313, F41G 700
Patent
active
052266141
ABSTRACT:
A portable missile launcher (12) has all of the infrared tracker (20) mounted to the same housing (48). The infrared missile beacon image beam (26) is intercepted by a rotating prism (28) which directs a portion of the beam to a narrow field detector (32) and reflects a further portion from a coating (30) onto a wide field detector (34). The detectors (32,34) provide yaw and pitch signals (40,42) which are compared with on-course information producing error signals communicated to the missile for course correction, if needed.
REFERENCES:
patent: 4202515 (1980-05-01), Maxwell, Jr.
patent: 4397429 (1983-08-01), Fouilloy
patent: 4407464 (1983-10-01), Linick
patent: 4967979 (1990-11-01), Balstad
patent: 5082201 (1992-01-01), Le Bars et al.
Brown C. D.
Denson-Low W. K.
Eldred J. Woodrow
Heald R. M.
Hughes Aircraft Company
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