Advances in dynamics and control of tethered satellite systems
From MaRDI portal
Publication:1939141
DOI10.1007/S10409-008-0159-9zbMath1257.70031OpenAlexW2090546122MaRDI QIDQ1939141
Dongping Jin, Haiyan Y. Hu, Hao Wen
Publication date: 26 February 2013
Published in: Acta Mechanica Sinica (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s10409-008-0159-9
Control of mechanical systems (70Q05) Orbital mechanics (70M20) Research exposition (monographs, survey articles) pertaining to mechanics of particles and systems (70-02)
Related Items (4)
Nonlinear dynamic analysis of a three-body tethered satellite system with deployment/retrieval ⋮ Chaotic motion analysis of a rigid spacecraft dragging a satellite by an elastic tether ⋮ Vibration and elastic wave propagation in spatial flexible damping panel attached to four special springs ⋮ De-spinning of tethered space target via partially invariable deployment with tension control
Cites Work
- Unnamed Item
- Optimal control of a tethered subsatellite of three degrees of freedom
- Optimal feedback control of the deployment of a tethered subsatellite subject to perturbations
- Deployment/retrieval optimization for flexible tethered satellite systems
- Optimal control of deployment of a tethered subsatellite
- Modelling, dynamics and control of tethered satellite systems
- Is the sky-hook configuration stable?
- Adaptive neural control of the deployment procedure for tether-assisted re-entry
- Three-dimensional optimal deployment of a tethered subsatellite with an elastic tether
- Tether applications in space transportation
- Controlled Dynamics of Flexible Orbiting Tethered Systems: Analysis and Experiments
- Dynamic behavior of electrodynamic tether deorbit system on elliptical orbit and its control by Lorentz force
- Dynamics and Control of Spinning Tethers for Rendezvous in Elliptic Orbits
- A targeting strategy for the deployment of a tethered satellite system
- Periodic Solutions and Controls of Tethered Systems in Elliptic Orbits
- Error-Tolerant Technique For Catching a Spacecraft With a Spinning Tether
- Dynamic simulation of a tethered satellite system using finite elements and fuzzy sets
This page was built for publication: Advances in dynamics and control of tethered satellite systems
