L1 Adaptive Control Integrated Missile Autopilot and Guidance-Reference-Cited by-同舟云学术

L1 Adaptive Control Integrated Missile Autopilot and Guidance

Published:2012-08-13 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
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Author:

Erdos David¹,Shima Tal¹,Kharisov Evgeny²,Hovakimyan Naira²

Affiliation:

1. Technion--Israel Institute of Technology

2. University of Illinois, Urbana-Champaign

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-4465

Reference16 articles.

1. 1Boskovic,J.D.andKnoebel,N."AComparisonStudyofSeveralAdaptiveControlStrategiesforResilientFlightControl,"Proceedingsof theAIAAGuidance,Navigation,andControlConference,No.August,Chicago,Illinois,2009,pp.1-22.

2. 2Lin, C. F., Wang, Q., Speyer, J. L., Evers, J. H., and Cloutier, J. R. "Integrated Estimation, Guidance, and Control System Design Using GameTheoreticApproach,"AmericanControlConference,1992,IEEE,Chicago,Illinois,1992,pp.3220-3224.

3. 3Menon,P.andOhlmeyer,E."IntegratedDesignofAgileMissileGuidanceandAutopilotSystems,"ControlEngineeringPractice,Vol.9, No.10,Oct.2001,pp.1095-1106. doi: 10.1016/S0967-0661(01)00082-X.

4. Adaptive flight control design for nonlinear missile

5. 5Kin,S.H.,Kim,Y.S.,andSong,C."ARobustAdaptiveNonlinearControlApproachtoMissileAutopilotDesign,"ControlEngineering Practice,Vol.12,No.2,Feb.2004,pp.149-154. doi: 10.1016/S0967-0661(03)00016-9.

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