Parametric Synthesis of Modal Control with Output Feedback for Descent Module Attitude Stabilization

Author(s):  
Alexey V. Lapin ◽  
Nikolay E. Zubov
Micromachines ◽  
2015 ◽  
Vol 6 (8) ◽  
pp. 993-1022
Author(s):  
José Guerrero-Castellanos ◽  
Hala Rifaï ◽  
Nicolas Marchand ◽  
Rafael Cruz-José ◽  
Samer Mohammed ◽  
...  

1976 ◽  
Vol 24 (2) ◽  
pp. 209-216 ◽  
Author(s):  
P. N. PARASKEVOPOULOS

Author(s):  
Yuquan Xia ◽  
Yuxin Su

The finite-time attitude stabilization of spacecraft subject to actuator constraints and attitude measurements only is investigated. A saturated output feedback finite-time proportional-derivative control is proposed. Lyapunov stability theory and homogeneous method are employed to show the finite-time stabilization. Advantages of the proposed control include the finite-time stabilization featuring faster transient and higher precision and the absence of the modelling information and the velocity measurements in the control law formulation, and thus, it offers an easy-going solution for high-quality motion control of spacecraft. An additive feature is that the actuator saturation will not be reached by selecting the control gains a priori. Simulations are presented to illustrate the effectiveness of the proposed control.


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