Aircraft modal suppression system

Aeronautics and astronautics – Aircraft control – Automatic

Patent

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244194, B64L 1316

Patent

active

050728938

ABSTRACT:
Accelerations due to excitation of the natural modes of an aircraft's body are suppressed by an active suppression system. Dedicated accelerometers are positioned in the aircraft at optimal locations for sensing modal induced lateral accelerations. The accelerometer produced signals are processed through control logic which, in response thereto, and in response to aircraft velocity and altitude related signals produces output control signals. The control signals effect rudder deployment creating forces to suppress the natural mode induced accelerations.

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patent: 3079108 (1963-02-01), Falkner et al.
patent: 3240447 (1966-03-01), Olshausen
patent: 3347498 (1967-10-01), Prietley et al.
patent: 3374966 (1968-03-01), Howard
patent: 3902686 (1975-09-01), Wykes

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