Design of midcourse guidance laws via a combination of fuzzy and SMC approaches-Reference-Cited by-同舟云学术

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Design of midcourse guidance laws via a combination of fuzzy and SMC approaches

Published:2010-04 Issue:2 Volume:8 Page:272-278
ISSN:1598-6446
Container-title:International Journal of Control, Automation and Systems
language:en
Short-container-title:Int. J. Control Autom. Syst.

Author:

Chen Chun-Hone,Liang Yew-Wen,Liaw Der-Cherng,Chang Shih-Tse,Xu Sheng-Dong

Publisher

Springer Science and Business Media LLC

Subject

Computer Science Applications,Control and Systems Engineering

Link

http://link.springer.com/content/pdf/10.1007/s12555-010-0213-9.pdf

Reference26 articles.

1. B. T. Burchett, “Feedback linearization guidance for approach and landing of reusable Launch Vehicles,” Proc. of American Control Conference, Portland, OR, USA, June 8–10, 2005.

2. A. Das, R. Das, S. Mukhopadhyay, and A. Patra, “Sliding mode controller along with feedback linearization for a nonlinear missile model,” Proc. of the 1st International Symposium on Syst. and Control in Aerospace and Astronautics, 2006.

3. D.-C. Liaw, Y.-W. Liang, and C.-C. Cheng, “Nonlinear control for missile terminal guidance,” ASME Journal of Dynamic Systems, Measurement and Control, vol. 122, pp. 663–668, Dec. 2000.

4. F.-K. Yeh, K.-Y. Cheng, and L.-C. Fu, “Variable structure-based nonlinear missile guidance/ autopilot design with highly maneuverable actuators,” IEEE Trans. Control Systems Technology, vol. 12, no. 6, pp. 944–949, Nov. 2004.

5. F.-K. Yeh, H.-H. Chien, and L.-C Fu, “Design of optimal midcourse guidance sliding-mode control for missiles with TVC,” IEEE Trans. on Aerospace and Electronic Systems, vol. 39, no. 3, pp. 824–837, 2003.

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