Robust Missile Autopilots With Finite-Time Convergence
Author:
Funder
National Natural Science Foundation of China
Publisher
Wiley
Subject
Control and Systems Engineering
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1002/asjc.1183/fullpdf
Reference30 articles.
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4. Missile autopilot design via a modified LPV synthesis technique;Biannic;Aerosp. Sci. Technol.,1999
5. Systematic gain-scheduling control design: A missile autopilot example;Wu;Asian J. Control,2002
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