Autonomous Hovering Proportional-Integral Sliding Mode Controller Design and Its Flight Test Validation for a Small-Scaled Unmanned Helicopter-Reference-Cited by-同舟云学术

Autonomous Hovering Proportional-Integral Sliding Mode Controller Design and Its Flight Test Validation for a Small-Scaled Unmanned Helicopter

Published:2013-10 Issue:4 Volume:26 Page:750-767
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Lin Chien-Hong¹,Jan Shau-Shiun²

Affiliation:

1. Ph.D. Student, Institute of Aeronautics and Astronautics, National Cheng Kung Univ., Tainan 70101, Taiwan.

2. Professor, Institute of Aeronautics and Astronautics, National Cheng Kung Univ., Tainan 70101, Taiwan (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000189

Reference21 articles.

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3. The novel adaptive sliding mode position control synchronous reluctance motor drive;Chen C. A.;J. Chinese Soc. Mech. Eng.,2008

4. Corban J. E. Calise A. Prasad J. Heynen G. Koenig B. and Hur J. (2003). “Flight evaluation of an adaptive velocity command system for unmanned helicopters.” Proc. AIAA Guidance Navigation and Control Conf. American Institute of Aeronautics and Astronautics Reston VA No. AIAA-2003-5594.

5. Hess R. A. and Wells S. R. (2002). “Sliding mode control applied to reconfigurable flight control design.” Proc. 40th AIAA Aerospace Sciences Meeting and Exhibit American Institute of Aeronautics and Astronautics Reston VA 1–12.

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