Low-thrust propulsion in a coplanar circular restricted four body problem

This paper formulates a circular restricted four body problem (CRFBP), where the three primaries are set in the stable Lagrangian equilateral triangle configuration and the fourth body is massless. The analysis of this autonomous coplanar CRFBP is undertaken, which identifies eight natural equilibri...

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Veröffentlicht in:	Celestial mechanics and dynamical astronomy 2012-02, Vol.112 (2), p.191-219
Hauptverfasser:	Ceccaroni, Marta, Biggs, James
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerospace Technology and Astronautics Asteroids Astrophysics Astrophysics and Astroparticles Classical Mechanics Dynamical Systems and Ergodic Theory Geophysics/Geodesy Numerical analysis Orbits Original Article Physics Physics and Astronomy Spacecraft Stability analysis
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