Nonlinear Discrete-time Design Methods for Missile Flight Control Systems-Reference-Cited by-同舟云学术

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Nonlinear Discrete-time Design Methods for Missile Flight Control Systems

Published:2004-06-22 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference and Exhibit
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Author:

Menon P.¹,Sweriduk Gregory¹,Vaddi S.¹,Ohlmeyer Ernest²

Affiliation:

1. Optimal Synthesis Inc.

2. Naval Surface Warfare Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-5326

Reference19 articles.

1. 1Ogata,K.,Discrete-TimeControlSystems,Prentice-Hall,UpperSaddleRiver,NJ,1995.

2. 3Slotine,J.E.,andLi,W.,AppliedNonlinearControl,Prentice-Hall,EnglewoodCliffs,NJ,1991.

3. 4Isidori,A.,NonlinearControlSystems,Springer-Verlag,NewYork,NY,1985.

4. 5Marino,R.,Tomei,P.,ControlDesign:Geometric,AdaptiveandRobust,Prentice-Hall,NewYork,NY,1995.

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