Title :
Bank-to-Turn Utilizing Sampled Data Non-Linear Control
Author :
Caughlin, D. ; Bullock, T.
Author_Institution :
Director, F-16XL Combined Test Force, Edwards Air Force Base, California 93523-5000
Abstract :
This paper discusses some of the aspects of bank-to-turn guidance utilizing Real-Time Sampled Data Non-Linear Control. The control law, first demonstrated on a six degree of freedom first order simulation, has been incorporated into a large, high fidelity, bank-to-turn missile simulation at the University of Florida. This paper outlines the Real-Time Sampled Data Non-Linear Control Algorithm. Trajectories using Real-Time Sampled Data Non-Linear Control will be presented at the conference.
Keywords :
Acceleration; Aerodynamics; Control systems; Error correction; Force control; Missiles; Nonlinear control systems; Optimal control; Real time systems; Testing;
Conference_Titel :
American Control Conference, 1986
Conference_Location :
Seattle, WA, USA