A Method for Deducing the Formulas of the Range Angle and the Flying Time with the Elliptical Orbit

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A Method for Deducing the Formulas of the Range Angle and the Flying Time with the Elliptical Orbit
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Abstract:

The range angle and the flying time for the passive section are calculated by using the quality with a constant vector in the direction of the major axis of the elliptical orbit in this paper.

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Niu Yun. A Method for Deducing the Formulas of the Range Angle and the Flying Time with the Elliptical Orbit[J]. Journal of National University of Defense Technology,1990,12(2):55-57.

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Received:August 05,1989
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Online: July 04,2015
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