Stability augmentation systems

Details Stability augmentation systems Stability augmentation systems

G - Physics

05

D

341/85

G05D 1/00 (2006.01) G05D 1/08 (2006.01)

Patent

CA 1081828

IMPROVEMENTS TO STABILITY AUGMENTATION SYSTEMS Abstract of the Disclosure: The gain of a stability augmentation system for an aircraft, particularly a helicopter, is automatically varied in accordance with the gross weight and deviations of the center of gravity of the aircraft. Gross weight and center of gravity are identified from in-flight measurements of collective and cyclic pitch stick position and airspeed. The gain of the stability augmentation system will not be changed during periods when the aircraft is being maneuvered.

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