NASA NTRS · 19920000265
Decoupling Control For Oblique-Wing Airplane
Abstract
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.
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Kempel, Robert W., Pahle, Joseph W., Alag, Gurbux S.. 1992-04-01. Decoupling Control For Oblique-Wing Airplane. https://ntrs.nasa.gov/citations/19920000265
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