Constant-Power Engines in Flights to L4 point of the Earth-Moon System
The transfer is studied in the context of the classical Circular Restricted Three-Body Problem. The initial state is on a geosinchronous orbit and the terminal state is the L4 triangular Lagrangian point. The use of controllable acceleration engine by minimization of a time integral of the squared e...
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| Format: | Article |
| Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2012-03-01
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| Series: | INCAS Bulletin |
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| Online Access: | http://bulletin.incas.ro/files/dumitrache_m__v4_iss_1_full.pdf |