Guidance processor

Details Guidance processor Guidance processor

1984-09-26

1993-10-19

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

F41G 700

Patent

active

052538230

ABSTRACT:
The invention relates to a guidance processor for a homing missile having a strapdown seeker providing sight line look angle measurements with respect to missile body axes and includes means for receiving sight line look angle measurements, and means for transforming the look angle measurements from missile body axes to pseudo measurements in a further set of axes defined to force the pseudo measurements to be small.

REFERENCES:
patent: 4396878 (1983-08-01), Cole et al.
patent: 4492352 (1985-01-01), Yueh
patent: 4494202 (1985-01-01), Yueh
patent: 4502650 (1985-03-01), Yueh
patent: 4508293 (1985-04-01), Jones

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