DocumentCode :
1795224
Title :
Finite-time stabilization-based trajectory tracking under disturbances for entry vehicles
Author :
Chen Dong ; Song-yan Wang ; Tao Chao ; Ming Yang
Author_Institution :
Control & Simulation Center, Harbin Inst. of Technol., Harbin, China
fYear :
2014
fDate :
8-10 Aug. 2014
Firstpage :
1943
Lastpage :
1948
Abstract :
For the entry guidance based on a nominal trajectory, trajectory tracking is an important part, by which the nominal trajectory is followed and several constraints can be observed. In order to reject disturbance and achieve good tracking performance in trajectory tracking, a finite-time trajectory tracking method is presented. Utilizing the differential flatness theory, a linear tracking error system can be derived from the nonlinear point-mass dynamics of an entry vehicle. A disturbance compensator is designed based on linear extended state observers. The compensator observes the disturbances in the tracking error system, and then compensates the disturbances in the following tracking law. To track the nominal trajectory, a finite-time tracking law with disturbance compensation is derived using a linear finite-time stabilization method. This method ensures that the tracking error is finite-time stable and the settling time of the tracking error is within a specified range. Numerical simulation demonstrates the proposed trajectory tracking law. Under various disturbances, good tracking performance is achieved and all constraints are observed. The proposed trajectory tracking method is effective.
Keywords :
entry, descent and landing (spacecraft); observers; space vehicles; stability; trajectory control; differential flatness theory; disturbance compensation; entry vehicles; finite-time stabilization-based trajectory tracking method; linear extended state observers; linear tracking error system; nominal trajectory; nonlinear point-mass dynamics; Aerodynamics; Closed loop systems; Target tracking; Trajectory; Vectors; Vehicle dynamics; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4799-4700-3
Type :
conf
DOI :
10.1109/CGNCC.2014.7007476
Filename :
7007476
Link To Document :
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