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Volume 1 (2008)

Keywords = Modified equinoctial orbital elements

Number of Articles: 1
Optimal Low Thrust Orbit Transfer Using Direct Collocation Method

R. Jamilnia; A. Naghash

Volume 1, Issue 2 , December 2008, , Pages 35-42

Abstract
  In this paper, a new approach is proposed for solving the problem of optimal low thrust orbit transfer. In this approach, the problem of trajectory optimization of optimal orbit transfer is defined by modified equinoctial orbital elements. For solving this problem, direct collocation method, that is ...  Read More