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Author = A. Ebrahimi

Number of Articles: 1
Optimal Control of Low Propulsion Orbital Transfer Time

A. Ebrahimi; H. R. Fayazbakhsh

Volume 4, Issue 1 , July 2011, , Pages 23-28

Abstract
  Within operational life of satellites according to their mission, need to change their operational orbits. This change can includes change in semi-major axis, inclination or plane of orbit (RAAN angle). For this propose, we can use Electrical Propulsion (EP). With respect to light weight of EP in cases ...  Read More