Pitch attitude stabilization system utilizing engine pressure ra

Details Pitch attitude stabilization system utilizing engine pressure ra Pitch attitude stabilization system utilizing engine pressure ra

1979-02-28

1981-05-12

Miller, J. D.

Aeronautics and astronautics

Aircraft control

Automatic

244181, G05D 108

Patent

active

042667437

ABSTRACT:
An aircraft pitch attitude stabilization system that utilizes an engine pressure ratio signal to cancel pitching moments due to changes in engine thrust. The changes in the engine pressure ratio signals which result from thrust changes are used to generate a pitch stabilization signal that is combined with other pitch control signals to automatically counteract pitching moments resulting from the changes in engine thrust.

REFERENCES:
patent: 3160367 (1964-12-01), Lecarme
patent: 3691356 (1972-09-01), Miller
patent: 3813063 (1974-05-01), Martin
patent: 3860800 (1975-01-01), Simpson

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