Periodic Optimal Control of a Spinning Earth-Pointing Tethered Satellite Formation-Reference-Cited by-同舟云学术

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Periodic Optimal Control of a Spinning Earth-Pointing Tethered Satellite Formation

Published:2006-06-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA/AAS Astrodynamics Specialist Conference and Exhibit
language:
Short-container-title:

Author:

Williams Paul¹

Affiliation:

1. RMIT University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-6764

Reference33 articles.

1. Williams,T.,andMoore,K."DynamicsofTetheredSatelliteFormations,"AAS/AIAASpace FlightMechanicsMeeting,Jan.27-30,2002,SanAntonio,TX,PaperAAS02-198.

2. Orbital Design of Earth-Oriented Tethered Satellite Formations

3. Dynamics of a Multi-Tethered Satellite Formation

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1. Stability Research of a Triangular Tethered Satellite Formation: Dynamics, Filtering, and Control;IEEE Transactions on Aerospace and Electronic Systems;2022-12

2. Robust control of triangular tethered satellite formation with unmeasured velocities;Acta Astronautica;2021-09

3. Formation-Keeping Control of the Closed-Chain System;Theory and Applications of Multi-Tethers in Space;2019-11-19

4. Configuration maintaining control of three-body ring tethered system based on thrust compensation;Acta Astronautica;2016-06

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