Optimization of short-time/three-impulse lambert rendezvous using interval analysis

来源 :The 4th International Conference on Dynamics, Vibration and | 被引量 : 0次 | 上传用户：zhaoyu_hit

【摘要】

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【作者】

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Hongliang Ma Shijie Xu

【机构】

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Beihang University, Beijing, PR China

【出处】

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The 4th International Conference on Dynamics, Vibration and

【发表日期】

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2014年8期

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To reduce the optimal but large AV of fixed short time Lambert rendezvous between two spacecraft along two coplanar circular orbits, a three-impulse Lambert rendezvous using interval analysis optimization is proposed in this paper.The purpose of optimization is to minimize the velocity increment of two Lambert transfer.Interval optimization algorithm is given for solving the rendezvous optimization problem with multiple uncertain variables and strong nonlinearity and nonconvexity.

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Optimization of short-time/three-impulse lambert rendezvous using interval analysis

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