The purpose of this paper is to summarize results obtained for the adaptive control of the F-8C aircraft using the so-called Multiple Model Adaptive Control method. The discussion includes the selection of the performance criteria for both the lateral and the longitudinal dynamics, the design of the Kalman filters for different flight conditions, the 'identification' aspects of the design using hypothesis testing ideas, and the performance of the closed loop adaptive system.
The stochastic control of the F-8C aircraft using the Multiple Model Adaptive Control (MMAC) method
IEEE Conf. on Decision and Control 1975 ; 1975 ; Houston, TX, United States
1975-08-01
Conference paper
No indication
English