DocumentCode :
3484284
Title :
Nonlinear optimal feedback control for lunar module soft landing
Author :
Zhou, Jingyang ; Zhou, Di ; Teo, Kok Lay ; Zhao, Guohui
Author_Institution :
Dept. of Control Sci. & Eng., Harbin Inst. of Technol., Harbin, China
fYear :
2009
fDate :
5-7 Aug. 2009
Firstpage :
681
Lastpage :
685
Abstract :
In this paper, the optimal control problem to achieve lunar module soft landing with least fuel consumption is considered. The precise three dimensional dynamics is employed to describe the motion of the lunar module. By introducing two new state equations, a closed loop optimal control law is designed with a parameter matrix K to be determined which is the solution of a riccati like differential equation. We present a practical method to calculate the matrix K, such that it is avoided to solve the complex riccati like differential equation. Simulation results show the efficiency of the proposed method.
Keywords :
aerospace control; closed loop systems; control system synthesis; matrix algebra; nonlinear control systems; optimal control; vehicle dynamics; closed loop optimal control law; lunar module soft landing; nonlinear optimal feedback control; riccati like differential equation; three dimensional dynamics; Automation; Differential equations; Feedback control; Fuels; Logistics; Mathematics; Moon; Optimal control; Riccati equations; Statistics; Feedback control; Lunar module; Soft landing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Automation and Logistics, 2009. ICAL '09. IEEE International Conference on
Conference_Location :
Shenyang
Print_ISBN :
978-1-4244-4794-7
Electronic_ISBN :
978-1-4244-4795-4
Type :
conf
DOI :
10.1109/ICAL.2009.5262838
Filename :
5262838
Link To Document :
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