Aeronautics and astronautics – Missile stabilization or trajectory control – Stabilized by rotation
Patent
1975-08-05
1977-05-31
Engle, Samuel W.
Aeronautics and astronautics
Missile stabilization or trajectory control
Stabilized by rotation
244 32, F42B 1514, F42B 1330, F42B 1510, F41G 900
Patent
active
040264980
ABSTRACT:
A sensor system that measures flight motions with respect to a classical Euler angle system of coordinates by aligning itself with the plane of total angle of attack via a pendulum mass. The system permits a simple determination of lift and drag for a spinning vehicle at angle of attack whereby the measurements are used as inputs to a flight control system to control the motions of the spinning vehicle.
REFERENCES:
patent: 3233848 (1966-02-01), Burne
patent: 3411736 (1968-11-01), Kelly
Engle Samuel W.
Rusz Joseph E.
Tashjian Arsen
The United States of America as represented by the Secretary of
Webb Thomas H.
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