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Motion Control of Electric Propulsion Spacecraft Transfers between the Libration Points L1 and L2 of the Earth–Moon System
| Authors: Fain M.K., Starinova O.L. | Published: 26.11.2019 |
| Published in issue: #11(716)/2019 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: spacecraft, low thrust engine, sequential linearization method, Earth–Moon system, libration point |
