Integrated Finite-Time Disturbance Observer and Controller Design for Reusable Launch Vehicle in Reentry Phase-Reference-Cited by-同舟云学术

Integrated Finite-Time Disturbance Observer and Controller Design for Reusable Launch Vehicle in Reentry Phase

Published:2017-01 Issue:1 Volume:30 Page:04016076
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Dong Qi¹,Zong Qun²,Tian Bailing³,Wang Fang⁴

Affiliation:

1. Ph.D. Candidate, College of Electric Engineering and Automation, Tianjin Univ., Tianjin 300072, China.

2. Professor, College of Electric Engineering and Automation, Tianjin Univ., Tianjin 300072, China.

3. Associate Professor, College of Electric Engineering and Automation, Tianjin Univ., Tianjin 300072, China (corresponding author).

4. Postdoctoral, School of Science, Yanshan Univ., Qinhuangdao, Hebei 066004, China.

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.1943-5525.0000670

Reference39 articles.

1. Quadrotor vehicle control via sliding mode controller driven by sliding mode disturbance observer

2. Bevacqua T. Best E. Huizenga A. Cooper D. and Zhu J. J. (2004). “Improved trajectory linearization flight controller for reusable launch vehicles.” Proc. 42nd AIAA Aerospace Science Meeting AIAA Reston VA.

3. Bialy B. J. Klotz J. Curtis J. W. and Dixon W. E. (2012). “An adaptive backstepping Controller for a hypersonic air-breathing missile.” Proc. AIAA Guidance Navigation and Control Conf. AIAA Reston VA 4468–4477.

4. Bollino K. P. (2006). “High-fidelity real-time trajectory optimization for reusable launch vehicles.” Ph.D. thesis Naval Postgraduate School Monterey CA.

5. Reentry Flight Controller Design Using Nonlinear Dynamic Inversion

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