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-Reference-Cited by-同舟云学术

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

Published:2007-08 Issue:4 Volume:45 Page:339-347
ISSN:0010-9525
Container-title:Cosmic Research
language:en
Short-container-title:Cosmic Res

Author:

Grigoriev I. S.,Grigoriev K. G.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering

Link

http://link.springer.com/content/pdf/10.1134/S0010952507040077.pdf

Reference48 articles.

1. Pontryagin, S.L., Boltyanskii, V.G., Gamkrelidze, R.V., and Mishchenko, E.F., Matematicheskaya teoriya optimal’nykh protsessov (Mathematical Theory of Optimal Processes), Moscow: Nauka, 1969.

2. Alekseev, V.M., Tikhomirov, V.M., and Fomin, S.V., Optimal’noe upravlenie (Optimal Control), Moscow: Nauka, 1979.

3. Galeev, E.M. and Tikhomirov, V.M., Kratkii kurs teorii ekstremal’nykh zadach (A Concise Course of Extreme Problems Theory), Moscow, 1989.

4. Grodzovskii G.L., Ivanov Yu.N., Tokarev V.V., Mekhanika kosmicheskogo poleta s maloi tyagoi (Mechanics of Low-Thrust Space Flight), Moscow: Nauka, 1966.

5. Ivashkin, V.V., Optimizatsiya kosmicheskikh manevrov pri ogranicheniyakh na rasstoyaniya do planet (Optimization of Space Maneuvers under Constraints on the Distances to Planets), Moscow: Nauka, 1975.

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