Adaptive autopilot

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

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Details

244 76C, 244191, F42B 1501

Patent

active

052481140

ABSTRACT:
An autopilot system including parameter identification circuits wherein the function of the torque and the function of the translational force on a missile are unknown and varying (including approaching zero).

REFERENCES:
patent: 3188019 (1965-06-01), Boutin
patent: 3362658 (1968-01-01), Ito et al.
patent: 3412960 (1968-11-01), Kocher et al.
patent: 3415215 (1968-12-01), Martin et al.
patent: 3497161 (1970-02-01), Kissinger et al.
patent: 3737122 (1973-06-01), Solov

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