Calculating Launch Windows for Transfers of Solar Powered EP Spacecraft between Low-earth Non-coplanar Circular Orbits

Author:

Ishkov S.A.,Petrukhina K.V.,Salmin V.V.

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference7 articles.

1. Popovich, P.R. Ballistic design of space systems. In Russian. Moscow, Mashinostroyenie, 1987, 240 pp.

2. “Non-coplanar inter-orbital transfers with low thrust electric propulsion, considering oscillations and requirements to orientation control system”. In Russian. Astronavtika i raketodinamika, 1975, Vol. 35, pp. 1-30.

3. Jonson, G.W. On a singular control problem in optimal rocket guidance [Text] /G.W. Jonson, D.H. Winfield. - AIAA Paper, №582. – 1967. - Pp. 1-7.

4. Kaufman H.R., Robinson R.C. Electric thruster performance for orbit raising maneuvering //AIAA Paper. 1982. № 1247. Pp. 1-9.

5. Graham K.F., Rao A.V. Minimum-Time Trajectory Optimization of Low-Thrust Earth-Orbit Transfers with Eclipsing //Journal of Spacecraft and Rockets, 2016. Volume 53, Issue 2. Pp. 289-303.

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