Analysis of the Structure of Families of Locally Optimum Solutions to the Problem of the Interplanetary Transfer of a Spacecraft with a Low-Thrust Engine-Reference-Cited by-同舟云学术

Analysis of the Structure of Families of Locally Optimum Solutions to the Problem of the Interplanetary Transfer of a Spacecraft with a Low-Thrust Engine

Published:2018-09 Issue:5 Volume:56 Page:365-372
ISSN:0010-9525
Container-title:Cosmic Research
language:en
Short-container-title:Cosmic Res

Author:

Vorobev A. L.,Elnikov R. V.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering

Link

http://link.springer.com/article/10.1134/S0010952518050076/fulltext.html

Reference11 articles.

1. Pontryagin, L.S., Boltyanskii, V.G., Gamkrelidze, R.V., and Mishchenko E.F., Matematicheskaya teoriya optimal’nykh protsessov (Mathematical Theory of Optimal Processes), Moscow: Nauka, 1976.

2. Melbourne, W.G. and Sauer, C.G., Optimum interplanetary rendezvous with power-limited vehicles, AIAA J., 1963, vol. 1, no. 1, pp. 54–60.

3. Melbourne, W.G. and Sauer, C.G., Optimum Earth–Mars roundtrip trajectories utilizing a low-thrust power-limited propulsion system, Adv. Astronaut. Sci., 1963, vol. 13, pp. 547–570.

4. Ivanov, Yu. N. and Shalaev, Yu.V., Steepest descent method to calculate the interorbital trajectories with power-limited vehicles, Kosm. Issled., 1964, vol. 2, no. 3, pp. 433–440.

5. Grodzovskii, G.L., Ivanov, Yu.N., and Tokarev, V.V., Mekhanika kosmicheskogo poleta. Problemy optimizatsii (Space Flight Mechanics. Optimization Problems), Moscow: Nauka, 1975.

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