Linearized Dynamics of Formation Flying Spacecraft on a J2-Perturbed Elliptical Orbit
Authors:
- 1 November 2007
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 30 (6) , 1649-1658
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Optimal Planner for Spacecraft Formations in Elliptical OrbitsJournal of Guidance, Control, and Dynamics, 2006
- Formation Design in Eccentric Orbits Using Linearized Equations of Relative MotionJournal of Guidance, Control, and Dynamics, 2006
- Cross-Track Motion of Satellite Formations in the Presence of J2 DisturbancesJournal of Guidance, Control, and Dynamics, 2005
- Relative Orbit Geometry Through Classical Orbit Element DifferencesJournal of Guidance, Control, and Dynamics, 2004
- Solution of the Elliptic Rendezvous Problem with the Time as Independent VariableJournal of Guidance, Control, and Dynamics, 2003
- High-Fidelity Linearized J Model for Satellite Formation FlightJournal of Guidance, Control, and Dynamics, 2002
- Relative Dynamics and Control of Spacecraft Formations in Eccentric OrbitsJournal of Guidance, Control, and Dynamics, 2002
- Satellite Formation Flying Design and EvolutionJournal of Spacecraft and Rockets, 2001
- Time-Explicit Representation of Relative Motion Between Elliptical OrbitsJournal of Guidance, Control, and Dynamics, 2000
- Motion in General Elliptic Orbit with Respect to a Dragging and Precessing Coordinate FrameThe Journal of the Astronautical Sciences, 1998