| 飞行器最优机动策略研究方法及进展 |
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| 引用本文： | 潘雷,谷良贤,高原.飞行器最优机动策略研究方法及进展[J].飞行力学,2009,27(4). |
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| 作者姓名： | 潘雷 谷良贤 高原 |
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| 作者单位： | 西北工业大学,航天学院,陕西,西安,710072 |
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| 基金项目： | 国家863计划资助项目(2007AA0897) |
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| 摘 要： | 回顾了国内外最优机动策略研究的理论和方法,着重论述了近几年国内外的最优轨道机动策略问题的研究状况,比较了国内外的发展差别,讨论了轨道最优机动策略的发展趋势,为我国飞行器最优轨道机动策略研究方向提供了有意义的参考。
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| 关 键 词： | 轨道机动 最优控制 机动策略 冲量型模型 有限推力 |
Development of Optimal Control Scheme in Orbit Maneuver of Flight Vehicles |
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| PAN Lei,GU Liang-xian,GAO Yuan.Development of Optimal Control Scheme in Orbit Maneuver of Flight Vehicles[J].Flight Dynamics,2009,27(4). |
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| Authors: | PAN Lei GU Liang-xian GAO Yuan |
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| Institution: | College of Astronautics;Northwestern Polytechnical University;Xi'an 710072;China |
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| Abstract: | The theory and development of the optimal control scheme in the trajectory optimization is reviewed in this paper.Its research fields in the recent years are introduced,and the gap between home and abroad is discussed.Finally,the trend of optimal control in the trajectory optimization is depicted,which will be an important guide to the development of an optimal orbit control scheme. |
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| Keywords: | orbit maneuver optimal control maneuver scheme impulsive model finite thrust |
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