Pulsed Optimal Spacecraft Orbit Reorientation by Means of Reactive Thrust Orthogonal to the Osculating Orbit. I-Reference-Cited by-同舟云学术

Pulsed Optimal Spacecraft Orbit Reorientation by Means of Reactive Thrust Orthogonal to the Osculating Orbit. I

Published:2018-09 Issue:5 Volume:53 Page:535-551
ISSN:0025-6544
Container-title:Mechanics of Solids
language:en
Short-container-title:Mech. Solids

Author:

Sapunkov Ya. G.,Chelnokov Yu. N.

Publisher

Allerton Press

Subject

General Physics and Astronomy,Mechanics of Materials

Link

http://link.springer.com/content/pdf/10.3103/S0025654418080083.pdf

Reference30 articles.

1. G. N. Duboshin, Celestial Mechanics: Basic Problems and Methods (Nauka, Moscow, 1968) [in Russian].

2. V. K. Abalakin, E. P. Aksenov, E. A. Grebenikov, et al., Reference Manual in Celestial Mechanics and Astrodynamics (Nauka, Moscow, 1976) [in Russian].

3. Yu. M. Kopnin, “On the Task of Rotating a Satellite’s Orbit Plane,” Kosm. Issl. 3 (4) (1965).

4. V. N. Lebedev, Calculation of Motion of a Spacecraft with Low Thrust (VTs AN, Moscow, 1968) [in Russian].

5. M. Z. Borshchevskii and M. V. Ioslovich, “On the Problem of Rotating the Orbital Plane of a Satellite by Means of Reactive Thrust,” Kosm. Issl. 7 (6) (1969).

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