Air Vehicle Flight Mechanism and Control Method
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United States of America Patent
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Mar 13, 2017
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Feb 9, 2001
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Abstract
Heavier-than-air, aircraft having flapping wings, e.g., ornithopters, where angular orientation control is effected by variable differential sweep angles of deflection of the flappable wings in the course of sweep angles of travel and/or the control of variable wing membrane tension.
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