Technical memorandum proposes procedure for mathematical synthesis of control signals proportional to commanded deflections of rudder, elevators, and ailerons of oblique-wing airplane. Procedure designed to generate signals compensating for aerodynamical and inertial cross-coupling among yawing, pitching, and rolling motions. Control interactions decoupled by feedforward and feedback.
Decoupling Control For Oblique-Wing Airplane
NASA Tech Briefs ; 16 , 4
1992-04-01
Miscellaneous
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English