Design concept of a tethered satellite cluster system-Reference-Cited by-同舟云学术

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Design concept of a tethered satellite cluster system

Published:2020-11 Issue: Volume:106 Page:106159
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Ma Yuechen,Ge Ruiqian,Xu Ming

Funder

National Natural Science Foundation of China

Foundation of Key Laboratory of Spacecraft Design Optimization and Dynamic Simulation Technologies, Ministry of Education of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference34 articles.

1. Space tether deployment control with explicit tension constraint and saturation function;Wen;J. Guid. Control Dyn.,2016

2. A review of space tether in new applications;Huang;Nonlinear Dyn.,2018

3. Nonlinear dynamics of a rotating triangular tethered satellite formation near libration points;Cai;Aerosp. Sci. Technol.,2015

4. Modeling issues related to retrieval of flexible tethered satellite systems;Kim;J. Guid. Control Dyn.,1995

5. Dynamic adaptive saturated sliding mode control for deployment of tethered satellite system;Ma;Aerosp. Sci. Technol.,2017

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2. Minimalistic estimation with stochastic constraints for closed-type tethered satellite formations;Aerospace Science and Technology;2023-10

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4. Framework Development for Efficient Mission-Oriented Satellite System-Level Design;Aerospace;2023-02-26

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