Deployment and retrieval of tethered satellite system under J2 perturbation and heating effect
Authors:
- B.S. YuBYB.S. Yu
- D.P. JinDJD.P. Jin
- 1 October 2010
- journal article
- Published by Elsevier in Acta Astronautica
- Vol. 67 (7-8) , 845-853
Abstract
No abstract availableKeywords
This publication has 14 references indexed in Scilit:
- Gravity modeling in aerospace applicationsAerospace Science and Technology, 2009
- Solar Pressure Effects for a Constellation in a Highly Elliptical OrbitJournal of Guidance, Control, and Dynamics, 2009
- Infinite-Horizon Control for Retrieving a Tethered Subsatellite via an Elastic TetherJournal of Guidance, Control, and Dynamics, 2008
- Linearized Dynamics of Formation Flying Spacecraft on a J2-Perturbed Elliptical OrbitJournal of Guidance, Control, and Dynamics, 2007
- Optimal feedback control of the deployment of a tethered subsatellite subject to perturbationsNonlinear Dynamics, 2007
- Optimal Control of a Tethered Subsatellite of Three Degrees of FreedomNonlinear Dynamics, 2006
- High-Fidelity Linearized J Model for Satellite Formation FlightJournal of Guidance, Control, and Dynamics, 2002
- Extension of tethered satellites in the atmosphereActa Astronautica, 2002
- Stability of a tethered satellite system1991
- Tethered aerothermodynamic research needsJournal of Spacecraft and Rockets, 1991