Trajectory Linearization Control Based Output Tracking Method for Nonlinear Uncertain System Using Linear Extended State Observer

Author:

Xingling Shao1,Honglun Wang2

Affiliation:

1. Unmanned Aerial Vehicle Research Institute; Beijing University of Aeronautics and Astronautics; Beijing 100191 China

2. Science and Technology on Aircraft Control Laboratory; Beijing University of Aeronautics and Astronautics; Beijing 100191 China

Publisher

Wiley

Subject

Control and Systems Engineering

Reference24 articles.

1. X-33 ascent flight control design by trajectory linearization: A singular perturbation approach;Zhu;Adv. Astron. Sci.,2001

2. Zhu , J. B. D. Banker C. E. Hall X-33 ascent flight controller design by trajectory linearization - a singular perturbational approach Proc. AIAA Guidance, Nav. and Ctrl. Conf 2000

3. Guidance, navigation, and control system design for tri-propeller vertical-takeoff-and-landing unmanned air vehicle;Huang;AIAA J Aircraft,2009

4. Zhu , B. W. Huo Adaptive trajectory linearization control for a model-scaled helicopter with uncertain inertial parameters Proc. Chinese Control Conf. 2012

5. Adami , T. M. J. Zhu 6DOF flight control of fixed-wing aircraft by trajectory linearization Proc. Amer. Control Conf. 2011

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