Automatic Landing System Design Using Multiobjective Robust Control-Reference-Cited by-同舟云学术

Automatic Landing System Design Using Multiobjective Robust Control

Published:2013-07 Issue:3 Volume:26 Page:603-617
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhao Lin¹,Yang Xuebo²,Gao Huijun³,Shi Peng⁴

Affiliation:

1. Graduate Student, Harbin Institute of Technology, Heilongjiang 150001, People’s Republic of China.

2. Lecturer, Harbin Institute of Technology, Heilongjiang 150001, People’s Republic of China (corresponding author).

3. Professor, Harbin Institute of Technology, Heilongjiang 150001, People’s Republic of China.

4. Professor, Univ. of Glamorgan, Pontypridd CF37 1DL, U.K., and Professor, Victoria Univ., Melbourne 8001, Australia.

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.1943-5525.0000174

Reference35 articles.

1. Robust Exact Pole Placement via an LMI-Based Algorithm

2. Linear Matrix Inequalities in System and Control Theory

3. Control of Spacecraft and Aircraft

4. Bryson A. E. Jr. and Zhao Y. (1987). “Feedback control for penetrating a downburst.” Technical Papers (A87-50401 22-08) AIAA Guidance Navigation and Control Conf. Vol. 1 American Institute of Aeronautics and Astronautics (AIAA) Reston VA 517–524.

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