Gu Xiaoqin. A Calculating Method for Epicyclic Motion of Spacecraft[J]. Journal of University of Electronic Science and Technology of China, 2003, 32(6): 635-637.
Citation: Gu Xiaoqin. A Calculating Method for Epicyclic Motion of Spacecraft[J]. Journal of University of Electronic Science and Technology of China, 2003, 32(6): 635-637.

A Calculating Method for Epicyclic Motion of Spacecraft

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  • Received Date: August 29, 2003
  • The analytic formulations are presented of the epicyclic motion of a spacecraft about the true anomaly and the eccentric anomaly. The eccentric anomaly as a function of time is calculated by the iterative method. And the iteration's convergence-condition is discussed. The relationship between the true anomaly and the time is gotten by the numerical integral method. The numerical simulation's results of this approach are presented.
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