A Research of the Technique of Optimizing the Orbit-alteration for the Exact-landing of Aerocraft by Using Evolution-algorithm

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A Research of the Technique of Optimizing the Orbit-alteration for the Exact-landing of Aerocraft by Using Evolution-algorithm
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This paper deals with the exact-landing of aerocraft and discusses a kind of the technique of optimizing the orbit-alteration for the exact-landing of aerocraft by using evolution-algorithm, based on single-pulse on orbital apogee and common single-pulse.

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ZHAO Jiankang, DAI Jinhai. A Research of the Technique of Optimizing the Orbit-alteration for the Exact-landing of Aerocraft by Using Evolution-algorithm[J]. Journal of National University of Defense Technology,2005,27(6):1-4.

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Received:September 18,2005
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Online: April 10,2013
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