吉林大学学报(工学版) ›› 2016, Vol. 46 ›› Issue (5): 1609-1615.doi: 10.13229/j.cnki.jdxbgxb201605033

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Adaptive supper-twisting control for spacecraft soft landing on asteroids

ZHANG Peng1,2, LIU Xiao-song1, DONG Bo3, LIU Ke-ping3, LI Yuan-chun1,3   

  1. 1.College of Communication Engineering, Jilin University, Changchun 130012, China;
    2.The 27st Research Institute of CETC,Zhengzhou 450047, China;
    3.College of Electrical and Electronic Engineering, Changchun University of Technology, Changchun 130012, China
  • Received:2015-06-13 Online:2016-09-20 Published:2016-09-20

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Abstract: In order to alleviate the chartering problem of the traditional sliding model control, an adaptive supper-twisting controller was designed for the spacecraft soft landing on asteroids. The controller has a simple algorithm structure and does not need to know the upper bound of the external disturbance's derivative. First, the control problem of soft landing was formulated as the stabilization of a nonlinear system. Second, a feedback control based on the spheric harmonic expansion model of the asteroid gravity was applied to decouple the system. Then, three adaptive supper-twisting controllers were designed to stabilize the subsystems. Simulations of soft landing on the Eros433 were performed to verify the effectiveness of the proposed controller. The simulation results were compared with the traditional adaptive sliding mode control to show the advantages of the proposed controller.

Key words: automatic control technology, soft landing on asteroids, adaptive super-twisting control, chattering attenuation, high-order sliding mode control

CLC Number: 

  • TP273
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