Analytic Approach and Landing Guidance through a Novel Time-Varying Sliding Mode Control Method-Reference-Cited by-同舟云学术

Analytic Approach and Landing Guidance through a Novel Time-Varying Sliding Mode Control Method

Published:2016-07 Issue:4 Volume:29 Page:04016008
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhao Yao¹,Sheng Yongzhi²,Liu Xiangdong³,Li Zhen⁴

Affiliation:

1. Ph.D. Candidate, School of Automation, Beijing Institute of Technology, Beijing 100081, China.

2. Lecturer, School of Automation, Beijing Institute of Technology, Beijing 100081, China (corresponding author).

3. Professor and Director, Key laboratory for Intelligent Control and Decision of Complex Systems, School of Automation, Beijing Institute of Technology, Beijing 100081, China.

4. Lecturer, School of Automation, Beijing Institute of Technology, Beijing 100081, 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.1943-5525.0000581

Reference23 articles.

1. A comment on ‘A time-varying sliding surface for fast and robust tracking control of second-order uncertain systems’

2. Time-varying sliding modes for second-order systems

3. Cloutier J. R. (1997). “State-dependent Riccati equation techniques: An overview.” Proc. American Control Conf. IEEE Albuquerque NM 932–936.

4. Exponential Time-varying Sliding Mode Control for Large Angle Attitude Eigenaxis Maneuver of Rigid Spacecraft

5. Hanson J. M. (2002). “A plan for advanced guidance and control technology for 2nd generation reusable launch vehicles.” Proc. AIAA Guidance Navigation and Control Conf. and Exhibit AIAA Monterey CA 1–9.

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