Minimum entropy control of closed-loop tracking errors for dynamic stochastic systems

2003 ◽  
Vol 48 (1) ◽  
pp. 118-122 ◽  
Author(s):  
Hong Yue ◽  
Hong Wang
Technometrics ◽  
1974 ◽  
Vol 16 (3) ◽  
pp. 391-398 ◽  
Author(s):  
George E. P. Box ◽  
John F. MacGregor

Author(s):  
Yiqi Xu

This paper studies the attitude-tracking control problem of spacecraft considering on-orbit refuelling. A time-varying inertia model is developed for spacecraft on-orbit refuelling, which actually includes two processes: fuel in the transfer pipe and fuel in the tank. Based upon the inertia model, an adaptive attitude-tracking controller is derived to guarantee the stability of the resulted closed-loop system, as well as asymptotic convergence of the attitude-tracking errors, despite performing refuelling operations. Finally, numerical simulations illustrate the effectiveness and performance of the proposed control scheme.


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