Adaptive Dynamic Surface Control for Integrated Missile Guidance and Autopilot in the Presence of Input Saturation-Reference-Cited by-同舟云学术

Adaptive Dynamic Surface Control for Integrated Missile Guidance and Autopilot in the Presence of Input Saturation

Published:2015-09 Issue:5 Volume:28 Page:04014121
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Liang Xiaoling¹,Hou Mingzhe²,Duan Guangren³

Affiliation:

1. Ph.D. Student, Center for Control Theory and Guidance Technology, School of Astronautics, Harbin Institute of Technology, Yikuang St., Harbin, Heilongjiang 150001, P.R. China.

2. Lecturer, Center for Control Theory and Guidance Technology, School of Astronautics, Harbin Institute of Technology, Yikuang St., Harbin, Heilongjiang 150001, P.R. China (corresponding author).

3. Professor, Center for Control Theory and Guidance Technology, School of Astronautics, Harbin Institute of Technology, Yikuang St., Harbin, Heilongjiang 150001, P.R. 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.1943-5525.0000458

Reference25 articles.

1. Proportional Guidance and CDM Control Synthesis for a Short-Range Homing Surface-to-Air Missile

2. Global Tracking Control of Underactuated Ships With Input and Velocity Constraints Using Dynamic Surface Control Method

3. Observer-based adaptive guidance law considering target uncertainties and control loop dynamics

4. Do H. M. Basar T. and Choi J. Y. (2004). “An anti-windup design for single input adaptive control systems in strict feedback form.” Proc. American Control Conf. Boston 2551–2556.

5. Backstepping-Based Flight Control with Adaptive Function Approximation

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