Missile maneuver concept

Registers – Transfer mechanism – Traveling pawl

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Details

23515025, 244 315, 244 32, G06F 1550, F42B 1502

Patent

active

040442373

ABSTRACT:
A lifting body missile is controlled by pitch and roll commands wherein the aw autopilot is caused to change in accordance with the roll and estimated angle of attack input information. A command logic is provided to determine the polarity of the command signals to the autopilot.

REFERENCES:
patent: 3301508 (1967-01-01), Yamron
patent: 3369772 (1968-02-01), Eberlein
patent: 3547381 (1970-12-01), Shaw et al.
patent: 3746281 (1973-07-01), Stripling
patent: 3951358 (1976-04-01), DeLano et al.

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