RSC Drug Discovery Series.
Royal Society of Chemistry.
Vol. 2017-January.
2017.
Spacecraft thrust vector control during landing on the moon surface
The problem of optimal control of the thrust vector of a spacecraft power engine, making a decay and soft landing from the circular satellite orbit of the Moon to its surface, is considered. The maximum principle of L.S.Pontryagin was used to determine the control structure. An approach has been developed to determine the optimal thrust control programs for the power engine. The results of the trajectory calculation of a spacecraft landing on the lunar surface are presented. © 2017 Univelt Inc. All rights reserved.
Authors
Matyushin M.M.1,
2
,
Ovechko V.M.1
,
Razoumny Y.N.
3
,
Skorobogatov O.P.1
,
Tyurina D.D.1
,
Baranova I.S.1
Publisher
Univelt Inc.
Language
English
Pages
181-188
Status
Published
Volume
161
Year
2017
Organizations
- 1 Central Research Institute of Machine, Mission Control Center, 4 Pionerskaya Str, Korolev, 141074, Russian Federation
- 2 Moscow Aviation Institute, 4, Volokalamskoe Ave, Moscow, 125993, Russian Federation
- 3 Peoples' Friendship University of Russia (RUDN University), 6 Mikluho- Maklaya Str, Moscow, 117198, Russian Federation
Keywords
Cobalt compounds; Dysprosium compounds; Engines; Lunar landing; Moon; Orbits; Vector control (Electric machinery); Water landing (spacecraft); Control structure; Lunar surface; Optimal controls; Satellite orbit; Spacecraft thrust vector control; Thrust control; Thrust vectors; Trajectory calculations; Sulfur compounds
Date of creation
19.10.2018
Date of change
21.04.2021
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