Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1988-12-19
1991-07-30
Sotomayor, John B.
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
342 53, 342 58, 342 62, F41G 732
Patent
active
050353756
ABSTRACT:
A fiber optic radar guided missile system 10 is disclosed which includes a radar receiver 12 disposed in a missile for receiving radar reflections and providing a first optical signal in response thereto. An optical receiver 14 is disposed at a launcher for receiving the first optical signal and for providing a set of electrical signals in response thereto. A fiber optic link 32 is connected between the missile and the launcher for communicating the first optical signal from the radar receiver 12 to the optical receiver 14.
In a specific embodiment, the invention 10 includes a first system 12 disposed in a missile for receiving radar reflections which includes only an antenna 16 for receiving radar reflections, a radar seeker 18 for providing a first electrical in response to the received radar reflections, and a first fiber optic transmitter 26 for converting the first electrical signal into a first optical signal. An optical receiver 14 is located at a launcher for receiving the first optical signal and for providing a set of electrical signals in response thereto. The optical receiver 14 at the launcher includes a first fiber optic receiver 48 for converting the first optical signal into a second electrical signal and a signal processor 56 for processing the second electrical signal and providing radar output data. A fiber optic link 32 is provided for communicating the first optical signal from the radar receiver 12 to the optical receiver 114 at the launcher and missile commands from the launcher to the missile.
REFERENCES:
patent: 3001186 (1961-09-01), Baltzer
patent: 3041011 (1962-06-01), Dhanes
patent: 3182930 (1965-05-01), Randolph, Jr. et al.
patent: 3729150 (1973-04-01), Conger
patent: 3743215 (1973-07-01), Harris
patent: 3891161 (1975-06-01), Hermann
patent: 3938148 (1976-02-01), Hobson
patent: 3943357 (1976-03-01), Culver
patent: 4185796 (1980-01-01), Riley
patent: 4611771 (1986-09-01), Gibbons et al.
patent: 4653032 (1987-03-01), Schwarz et al.
patent: 4705237 (1987-11-01), Goldfeld et al.
patent: 4770370 (1988-09-01), Pinson
patent: 4796833 (1989-01-01), Pinson
patent: 4860968 (1989-08-01), Pinson
patent: 4907763 (1990-03-01), Pinson
patent: 4967980 (1990-11-01), Pinson
patent: 4974793 (1990-12-01), Pinson
Electro 81 Conference Record, vol. 6, part 8c/3, 7-9 Apr. 1981, New York, NY, US, H. Wichansky et al., "Fiber Optic Implications for Missile Guidance Design", pp. 1-10, see whole document.
Revue Internationale De Defense, vol. 17, No. 2, 1984, Cointrin-Geneve CH, pp. 151-154, J. Rhea, "Utilisations Militaires des Fibres Optiques", see the whole document.
Milocom 86, 1986, IEEE Military Communications Conference, 5-9 Oct. 1986, Monteray, CA, Communications-Computers, Teamed for the '90s, Conference Record, vol. 2 of 3, IEEE, US-D. Biswas et al., "Fiber-optic Guidance for Missiles", pp. 3331-3335, see whole document.
de La Chapelle Michael
Friedenthal Kenneth J.
Hsu Hui-Pin
Brown C. D.
Denson-Low W. K.
Heald R. M.
Hughes Aircraft Company
Sotomayor John B.
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