scholarly journals Finite-time attitude tracking control design for reusable launch vehicle in reentry phase based on disturbance observer

2017 ◽  
Vol 9 (12) ◽  
pp. 168781401774407 ◽  
Author(s):  
Fang Wang ◽  
Qin Zou ◽  
Changchun Hua ◽  
Qun Zong
Author(s):  
Qun Zong ◽  
Xiuyun Zhang ◽  
Shikai Shao ◽  
Bailing Tian ◽  
Wenjing Liu

In this paper, finite-time fault-tolerant attitude tracking control is investigated for rigid spacecraft system with external disturbances, inertia uncertainties and actuator faults. A novel finite-time disturbance observer combined with a nonsingular terminal sliding mode controller is developed. Using an equivalent output error injection approach, a finite-time disturbance observer with simple structure is firstly designed to estimate lumped uncertainty. Then, to remove the requirement of prior knowledge about lumped uncertainty and reduce chattering, an adaptive finite-time disturbance observer is further proposed, and the estimations converge to the neighborhood of the true values. Based on the designed observer, a unified finite-time attitude controller is obtained automatically. Finally, both additive and multiplicative faults are considered for simulations and the results illustrate the great fault-tolerant capability of the proposed scheme.


2020 ◽  
Vol 31 (6) ◽  
pp. 1274-1285
Author(s):  
Shi Zhen ◽  
Xie Yaen ◽  
Deng Chengchen ◽  
Zhao Kun ◽  
He Yushan ◽  
...  

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