Biodynamic resistant control stick
AssigneeThe United States of America as represented by the Secretary of the Air Force
InventorDaniel W. Repperger
Life of this patent
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Abstract
An improvement to an aircraft control stick is disclosed. Movement of an aircraft may generate a force which undesirably causes the aircraft pilot to deflect the aircraft's control stick, which thereby results in the aircraft deviating from the desired flight path. The present invention includes a processor-based system which employs an algorithm that generates a signal for causing the control stick to resist such forces. The invention includes a spring and damper connected to the control stick so that the spring constant and damping ratio may be varied.
Claims5
An aircraft control system which comprises:
- (a) a pilot operable member pivotally connected to the aircraft and adapted so that movement thereof causes deflection of control surfaces of the aircraft;
- (b) a force sensor connected to the aircraft for generating a force signal proportional to a given force acting on the aircraft;
- (c) a processor embodying an algorithm capable of translating said force signal representing said given force acting on said aircraft into a processed signal representing a resistant force correlated with a particular biodynamic force generated by the aircraft pilot's arm on said pilot operable member due to said given force on said aircraft, said processor, upon receiving said force signal from said force sensor, being capable of performing said translation and generating said processed signal;
- (d) resilient means connected to the aircraft and to said pilot operable member;
- and
- (e) an actuator connected to the aircraft and to said pilot operable member by said resilient means, said actuator being capable of receiving said processed signal and, in response to said signal, of adjusting said resilient means so as to impose said resistant force upon said pilot operable member and null out said biodynamic force acting on said member induced by the action of said given force on the aircraft, as exerted through the arm of the aircraft pilot.
Dependencies are inferred from the claim text.