Improved Quadrotor Altitude Control Design Using Second-Order Sliding Mode-Reference-Cited by-同舟云学术

Improved Quadrotor Altitude Control Design Using Second-Order Sliding Mode

Published:2017-11 Issue:6 Volume:30 Page:04017065
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Nadda Sudhir¹,Swarup A.²

Affiliation:

1. Ph.D. Student, Dept. of Electrical Engineering, National Institute of Technology, Kurukshetra, Haryana 136119, India (corresponding author).

2. Professor, Dept. of Electrical Engineering, National Institute of Technology, Kurukshetra, Haryana 136119, India.

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.1943-5525.0000781

Reference25 articles.

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2. Bouabdallah S. and Siegwart R. (2005). “Backstepping and sliding mode techniques applied to an indoor micro quadrotor.” Proc. IEEE Int. Conf. on Robotics and Automation IEEE New York 2259–2264.

3. Bouadi H. Cunha S. S. Drouin A. and Mora-Camino F. (2011). “Adaptive sliding mode control for quadrotor attitude stabilization and altitude tracking.” Proc. 12th IEEE Int. Symp. on Computational Intelligence and Informatics IEEE New York 449–455.

4. Improved adaptive sliding mode control for rigid spacecraft attitude tracking;Cong B.;J. Aerospace Eng.,2014

5. Second order sliding mode control with experiment application;Eker L.;ISA Trans.,2010

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