中国空间科学技术

Chinese Space Science and Technology

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Rapid Searching Method for Optimal Close Approach Orbit under Statistic Conditions

Liu Luhua Zheng Wei Tang Guojian(College of Astronautical & Material Engineering,National University of Defense Technology,Changsha 410073)   

  • Online:2006-08-25

Abstract: The close approach analysis to surveilled satellites is necessary when designing a space surveillance satellite.Based on a simulation,a rapid optimal close approach orbit searching method is put forward.The simulation results approve the method is effective,and the statistic(parameters) are verified by the precise model.The creditability is validated either.