Solar sailing trajectory optimization with planetary gravity assist

来源 :中国科学：物理学、力学、天文学英文版 | 被引量 : 0次 | 上传用户：dlzhwp

【摘要】

：

Significant propellant mass saving can be obtained with the use of complex multiple intermediate flyby maneuvers for conventional propulsion systems,and trip ti

【作者】

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CAI XingShan LI JunFeng GONG S

【机构】

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SchoolofAerospace

【出处】

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中国科学：物理学、力学、天文学英文版

【发表日期】

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2015年1期

【关键词】

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太阳能轨迹优化帆船重力运动行星最优控制问题星历模型 solar sailing trajectory optimization gravity

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Significant propellant mass saving can be obtained with the use of complex multiple intermediate flyby maneuvers for conventional propulsion systems,and trip time also decreases for a portion of the proper solar sail missions.This paper discusses the perf

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Solar sailing trajectory optimization with planetary gravity assist

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