Guidance Laws With Input Constraints and Actuator Failures
Author:
Funder
the National Natural Science Foundation of China
Publisher
Wiley
Subject
Control and Systems Engineering
Reference23 articles.
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2. Tournes C. H. Y. B. Shtessel Integrated guidance and autopilot for dual controlled missiles using higher order sliding mode controllers and observers AIAA Paper 1 25 2008
3. Integrated higher-order sliding mode guidance and autopilot for dual control missiles;Shtessel;J. Guid. Control Dyn.,2009
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5. Adaptive nonlinear guidance law considering control loop dynamics;Chwa;IEEE Trans. Aerosp. Electron. Syst.,2003
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