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Tan Lifen Yan Ye Zhou Ying Tang Guojin(College of Aerospace and Material Engineering,National University of Defense Technology,Changsha 410073)
Online:
Abstract: The inclination will drift because of the inference of solar gravity perturbation and lunar gravity perturbation.The analytic equations for computation of long-term evolution of inclination of HEO with small inclination were deduced.The maintenance strategy of inclination was put forward.The deviation of the inclination,comparing with numeric results calculated by STK,was within 5% which indicate the preciseness of the deduced analytical equations.The simulation of inclination maintenance was also executed.The results show that the maintenance strategy of inclination is effective and the deduced analytical equations have good engineering prospect application.
Tan Lifen Yan Ye Zhou Ying Tang Guojin(College of Aerospace and Material Engineering,National University of Defense Technology,Changsha 410073). Long-term Evolution and Control of Inclination for High Eccentric Orbit[J]. .
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URL: http://journal26.magtechjournal.com/kjkxjs/EN/
http://journal26.magtechjournal.com/kjkxjs/EN/Y2010/V30/I03/37