This paper provides the dynamic model of the deployment of tether-assisted re-entry system include J2 perturbation based on Lagrange equation. Some qualitative analyses of J2 perturbation effect on the system are given based on the dynamic model: J2 perturbation effect will induce some offset according to the deployment track of the system. Then a mathematic simulation is provided to validate and analyze the J2 perturbation effect on the deployment of the system in free and exponential deployment scheme. The results showed that J2 perturbation can effect the movement of the system in-plane, but can’t induce the movement of the system out-of-plane.
J2 perturbation effect on the deployment of tether-assisted deorbit system
2008-12-01
700734 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Tether deorbit system - A promising alternative
AIAA | 1989
|The RETRIEVE Microsatellite Tether Deorbit Experiment
AIAA | 2002
|Optimization and Control of the Early Deployment Phase during a Tether-Assisted Deorbit Maneuver
British Library Conference Proceedings | 2000
|Terminator Tether: A Spacecraft Deorbit Device
AIAA | 2000
|