Continuous thrust tangential or perpendicular to the flight direction on a given transfer trajectory in planar Circular Restricted 3-Body Problem
This paper presents a systematic study for analytical determination of thrust acceleration magnitude on a given trajectory for a case where the thrust is tangential or perpendicular to the flight direction. The problem has been formulated using the planar Circular Restricted Three-Body Problem. In t...
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| Format: | Article |
| Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2011-06-01
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| Series: | INCAS Bulletin |
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| Online Access: | http://bulletin.incas.ro/files/dumitrache_mircea_v3_is2_full.pdf |
| _version_ | 1811324834784739328 |
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| author | Mircea DUMITRACHE |
| author_facet | Mircea DUMITRACHE |
| author_sort | Mircea DUMITRACHE |
| collection | DOAJ |
| description | This paper presents a systematic study for analytical determination of thrust acceleration magnitude on a given trajectory for a case where the thrust is tangential or perpendicular to the flight direction. The problem has been formulated using the planar Circular Restricted Three-Body Problem. In the numerical application for tangential thrust the transfer from low Earth orbit to planar Lyapunov orbits around L1 and L2 Lagrangian points by a semi-elliptic transfer path is considered. For the case in which the thrust is perpendicular to the flight direction also on a semi-elliptic trajectory, the results are compared to the ones of Miele and Mancuso (2001), and Sandro da Silva Fernandes (2010) in their studies based on a simplified version of the same restricted three-body problem of transferring a spacecraft from a circular low Earth orbit to a circular low Moon orbit. |
| first_indexed | 2024-04-13T14:22:29Z |
| format | Article |
| id | doaj.art-f891bfa8af73477691d50318156e269a |
| institution | Directory Open Access Journal |
| issn | 2066-8201 2247-4528 |
| language | English |
| last_indexed | 2024-04-13T14:22:29Z |
| publishDate | 2011-06-01 |
| publisher | National Institute for Aerospace Research “Elie Carafoli” - INCAS |
| record_format | Article |
| series | INCAS Bulletin |
| spelling | doaj.art-f891bfa8af73477691d50318156e269a2022-12-22T02:43:26ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282011-06-0132213410.13111/2066-8201.2011.3.2.3Continuous thrust tangential or perpendicular to the flight direction on a given transfer trajectory in planar Circular Restricted 3-Body ProblemMircea DUMITRACHEThis paper presents a systematic study for analytical determination of thrust acceleration magnitude on a given trajectory for a case where the thrust is tangential or perpendicular to the flight direction. The problem has been formulated using the planar Circular Restricted Three-Body Problem. In the numerical application for tangential thrust the transfer from low Earth orbit to planar Lyapunov orbits around L1 and L2 Lagrangian points by a semi-elliptic transfer path is considered. For the case in which the thrust is perpendicular to the flight direction also on a semi-elliptic trajectory, the results are compared to the ones of Miele and Mancuso (2001), and Sandro da Silva Fernandes (2010) in their studies based on a simplified version of the same restricted three-body problem of transferring a spacecraft from a circular low Earth orbit to a circular low Moon orbit.http://bulletin.incas.ro/files/dumitrache_mircea_v3_is2_full.pdfplanar Circular Restricted Three-Body Problemgiven trajectorycontinuous thrust controlEarth-Moon systemlow Moon orbitLagrangian points |
| spellingShingle | Mircea DUMITRACHE Continuous thrust tangential or perpendicular to the flight direction on a given transfer trajectory in planar Circular Restricted 3-Body Problem INCAS Bulletin planar Circular Restricted Three-Body Problem given trajectory continuous thrust control Earth-Moon system low Moon orbit Lagrangian points |
| title | Continuous thrust tangential or perpendicular to the flight direction on a given transfer trajectory in planar Circular Restricted 3-Body Problem |
| title_full | Continuous thrust tangential or perpendicular to the flight direction on a given transfer trajectory in planar Circular Restricted 3-Body Problem |
| title_fullStr | Continuous thrust tangential or perpendicular to the flight direction on a given transfer trajectory in planar Circular Restricted 3-Body Problem |
| title_full_unstemmed | Continuous thrust tangential or perpendicular to the flight direction on a given transfer trajectory in planar Circular Restricted 3-Body Problem |
| title_short | Continuous thrust tangential or perpendicular to the flight direction on a given transfer trajectory in planar Circular Restricted 3-Body Problem |
| title_sort | continuous thrust tangential or perpendicular to the flight direction on a given transfer trajectory in planar circular restricted 3 body problem |
| topic | planar Circular Restricted Three-Body Problem given trajectory continuous thrust control Earth-Moon system low Moon orbit Lagrangian points |
| url | http://bulletin.incas.ro/files/dumitrache_mircea_v3_is2_full.pdf |
| work_keys_str_mv | AT mirceadumitrache continuousthrusttangentialorperpendiculartotheflightdirectiononagiventransfertrajectoryinplanarcircularrestricted3bodyproblem |