Systematic Direct Approach for Optimizing Continuous-thrust Earth-orbit Transfers

ed solutions are obtained from simply defined initial guesses. The proposed direct approach is briefly compared with other methods. Finally, we discussed the potential onboard guidance scheme using model predictive control.

作 者： Gao Yang Li Weiqi   作者單位： Gao Yang(Academy of Opto-Electronics, Chinese Academy of Sciences, Beijing 100080, China)

Li Weiqi(School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China) 

刊 名： 中國航空學(xué)報(bào)（英文版）  ISTIC 英文刊名： CHINESE JOURNAL OF AERONAUTICS  年，卷(期)： 2009 22(1)  分類號(hào)： V2  關(guān)鍵詞： low-thrust   orbital transfer   optimization   multiple shooting   variable specific impulse   guidance scheme   model predictive control