Optimization of the interplanetary trajectories of spacecraft with a solar electric propulsion power plant of minimal power

Author:

Ivanyukhin A. V.,Petukhov V. G.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics

Reference14 articles.

1. Chernous’ko, F.L., Otsenivanie fazovogo sostoyaniya dinamicheskikh sistem (The Way to Estimate Phase State of Dynamical Systems), Moscow: Nauka, 1988.

2. Grigoriev, I.S. and Grigoriev, K.G., The use of solutions to problems of spacecraft trajectory optimization in impulse formulation when solving the problems of optimal control of trajectories of a spacecraft with limited thrust engine: I, Cosmic Res., 2007a, vol. 45, no. 4, pp. 339–347.

3. Grigoriev, I.S. and Grigoriev, K.G., The use of solutions to problems of spacecraft trajectory optimization in impulse formulation when solving the problems of optimal control of trajectories of a spacecraft with limited thrust engine: II, Cosmic Res., 2007b, vol. 45, no. 6, pp. 553–563.

4. Irving, J.H., Low thrust flight: variable exhaust velocity in gravitational fields, in Space Technology, Seifert, H., Ed., New York: Wiley, 1959, chap. 10.

5. Lyness, J.N., Numerical algorithms based on the theory of complex variables, Proc. 22nd ACM Nat. Conf., Washington: Thompson Book, 1967a, pp. 124–134.

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