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持续推进地球轨道转移的直接优化方法(英文) 被引量:5

Systematic Direct Approach for Optimizing Continuous-thrust Earth-orbit Transfers
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摘要 This article presents a systematic direct approach to carry out effective optimization of a wide range of continuous-thrust Earth-orbit transfers with intermediate-level thrust acceleration,including minimum-time (with a single burn arc) and mini-mum-fuel (with multiple burn arcs) transfers. With direct control parameterization,in which the control steering programs of burn arcs are interpolated through a finite number of nodes,the optimal control problem is converted into the parameter optimi-zation proble... This article presents a systematic direct approach to carry out effective optimization of a wide range of continuous-thrust Earth-orbit transfers with intermediate-level thrust acceleration,including minimum-time (with a single burn arc) and mini-mum-fuel (with multiple burn arcs) transfers. With direct control parameterization,in which the control steering programs of burn arcs are interpolated through a finite number of nodes,the optimal control problem is converted into the parameter optimi-zation proble...
作者 高扬 李卫琪
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2009年第1期56-69,共14页 中国航空学报(英文版)
基金 National Natural Science Foundation of China (10603005) Foundation of President of the Academy of Opto-Electro-nics ( AOE-CX-200601)
关键词 LOW-THRUST orbital transfer OPTIMIZATION multiple shooting variable specific impulse guidance scheme model pre-dictive control low-thrust orbital transfer optimization multiple shooting variable specific impulse guidance scheme model pre-dictive control
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  • 1M. J. H. Walker,B. Ireland,Joyce Owens. A set modified equinoctial orbit elements[J] 1985,Celestial Mechanics(4):409~419

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