Solar Sail Equilibria in the Elliptical Restricted Three-Body Problem
- 1 May 2006
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 29 (3), 538-543
- https://doi.org/10.2514/1.15596
Abstract
The existence and dynamical properties of artificial equilibria for solar sails in the elliptical restricted threebody problem is investigated.We show that planar two-dimensional equilibrium curves exist, embedded in threedimensional space, in a nonuniformly rotating, pulsating coordinate system. However, due to the stretching of the system plane coordinates and unstretching of the out-of-plane coordinate, the equilibrium surfaces do not exist in the three-dimensional elliptical restricted three-body system. Control in the neighborhood of an equilibrium point is investigated through a pole assignment scheme. This permits practical out-of-plane equilibria in elliptical three-body systems with small eccentricityKeywords
This publication has 10 references indexed in Scilit:
- Solar sailing: mission applications and engineering challengesPhilosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences, 2003
- Solar sailing: Orbital mechanics and mission applicationsAdvances in Space Research, 2003
- Solar Sail Orbit Operations at AsteroidsJournal of Spacecraft and Rockets, 2001
- Artificial Lagrange Points for a Partially Reflecting Flat Solar SailJournal of Guidance, Control, and Dynamics, 1999
- Mathematical Theory of Control Systems DesignPublished by Springer Science and Business Media LLC ,1996
- Solar sail parking in restricted three-body systemsJournal of Guidance, Control, and Dynamics, 1994
- Linear stability of the triangular equilibrium points in the photogravitational elliptic restricted problem, IIAstrophysics and Space Science, 1993
- Linear stability of the triangular equilibrium points in the photogravitational elliptic restricted problem, IAstrophysics and Space Science, 1992
- Statite - A spacecraft that does not orbitJournal of Spacecraft and Rockets, 1991
- The restricted 3-body problem with radiation pressureCelestial Mechanics and Dynamical Astronomy, 1985