Parameter identification and design of a robust attitude controller using H ∞ methodology for the raptor E620 small-scale helicopter-Reference-Cited by-同舟云学术

Parameter identification and design of a robust attitude controller using H ∞ methodology for the raptor E620 small-scale helicopter

Published:2012-02 Issue:1 Volume:10 Page:88-101
ISSN:1598-6446
Container-title:International Journal of Control, Automation and Systems
language:en
Short-container-title:Int. J. Control Autom. Syst.

Author:

Kim Ho-Chan,Dharmayanda Hardian Reza,Kang Taesam,Budiyono Agus,Lee Gigun,Adiprawita Widyawardana

Publisher

Springer Science and Business Media LLC

Subject

Computer Science Applications,Control and Systems Engineering

Link

http://link.springer.com/content/pdf/10.1007/s12555-012-0110-5.pdf

Reference39 articles.

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2. V. Gavrilets, B. Mettler, and E. Feron, “Nonlinear model for a small-size acrobatic helicopter,” Proceedings of the AIAA Guidance, Navigation and Control Conference, Montreal, Canada, Paper No. AIAA 2001-4333, 2001.

3. V. Gavrilets, I. Martinos, B. Mettler, and E. Feron, “Flight test and simulation results for an autonom ous aerobatic helicopter,” Proc. of AIAA/IEEE Digital Avionics Systems Conference, pp. 1423–1429, 2002.

4. H. J. Kim, D. H. Shim, and S. Sastry, “A flight control system for aerial robots: algorithms and experiments,” Control Engineering Practice, vol. 11, pp. 1389–1400, 2003.

5. T. J. Koo and S. Sastry, “Output tracking control design of a helicopter model based on approximate linearization,” Proc. of the 37th IEEE Conference on Decision and Control, Tampa, FL, USA, pp. 3635–3640, 1998.

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