Adaptive Integrated Guidance and Control Based on Backstepping and Input-to-State Stability
Author:
Publisher
Wiley
Subject
Control and Systems Engineering
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1002/asjc.682/fullpdf
Reference18 articles.
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3. Williams , D. E. J. Richman B. Friedland Design of an integrated strapdown guidance and control system for a tactical missile 1983
4. Integrated guidance and control for homing missiles against ground fixed targets;Hou;Chin. J. Aeronaut.,2008
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