Title :
Optimal Orbit Design of Lunar Modules Soft Landing
Author :
Zhou Jing-yang ; Zhou Di ; Duan Guang-Ren
Author_Institution :
Harbin Inst. of Technol., China
Abstract :
Precise three dimensional dynamics for lunar soft landing were presented. To realize the minimal fuel strategy, an optimal control law was proposed based on the maximum principle. By solving the two-point boundary value problem, the optimal trajectory of the lunar soft landing was obtained. Performance of the proposed control law was verified by simulation.
Keywords :
aerospace control; boundary-value problems; fuel optimal control; maximum principle; position control; boundary value problem; lunar module soft landing; maximum principle; minimal fuel strategy; optimal control law; optimal orbit design; optimal trajectory; Boundary value problems; Control systems; Fuels; IEEE catalog; Moon; Optimal control; Lunar Module; Optimal Trajectory; Soft Lading;
Conference_Titel :
Control Conference, 2006. CCC 2006. Chinese
Conference_Location :
Harbin
Print_ISBN :
7-81077-802-1
DOI :
10.1109/CHICC.2006.280951
