The theory and design of optimal adaptive control laws for automatic control of aircraft in the azimuth radio guidance system (instrument landing system) are presented. The control laws are developed using Pontryagin maximum principle with state dynamics and cost function. (Author)
Optimal-Adaptive Control Theory for Automatic Control of Aircraft
1972
44 pages
Report
Keine Angabe
Englisch
LQR-Based Adaptive Optimal Control for Aircraft Engine
Springer Verlag | 2023
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