Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1984-05-09
1986-03-18
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F41G 722
Patent
active
045763461
ABSTRACT:
In a seeker head for a target seeking missile, which comprises a seeker 28 adapted to be directed to a target, two distance sensors 32 and 34 in the form of laser transceiver units are adapted to be directed to the target together with the seeker 28. The arrangement of the distance sensors 32 and 34 on opposite sides of the pitch axis 26 ensures that, with large squint angles, at most one of the distance sensors 32 and 34 is covered.
REFERENCES:
patent: 3935818 (1976-02-01), Johnson et al.
patent: 3971939 (1976-07-01), Andressen
patent: 4168813 (1979-09-01), Pinson et al.
Eckhardt Reiner
Gauggel Roland
Bodenseewerk Geratetechnic GmbH
Jordan Charles T.
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