The development of a digital adaptive flight control algorithm is described that combines a weighted least squares estimator with optimal linear regulator control logic designed to minimize a quadratic model following performance index. Very promising results for a typical fighter aircraft's trajectory over six distinct flight conditions are reported.
Digital adaptive flight controller development
Conference on Decision and Control ; 1973 ; San Diego, CA, US
1973-01-01
Miscellaneous
No indication
English
Digital adaptive flight controller development
NTRS | 1974
|Digital Adaptive Flight Controller Development
NTIS | 1974
|Digital adaptive flight controller development
TIBKAT | 1974
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