Nonlinear Aircraft Flight Control Using Dynamic Inversion
Author :
Wise, Kevin A.
Author_Institution :
Staff Specialist, Advanced Guidance, Navigation and Control, McDonnell Douglas Missile Systems Company, Mailcode 3064045, P.O. Box 516, St. Louis, MO 63166
fYear :
1992
fDate :
24-26 June 1992
Firstpage :
1322
Lastpage :
1326
Keywords :
Acceleration; Aerodynamics; Aerospace control; Aircraft; Control design; Elevators; Force control; Missiles; Modems; Nonlinear equations;
