Stability and Control of a Flux-Pinned Docking Interface for Spacecraft-Reference-Cited by-同舟云学术

Stability and Control of a Flux-Pinned Docking Interface for Spacecraft

Published:2010-06-26 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
language:
Short-container-title:

Author:

Jones Laura¹,Peck Mason¹

Affiliation:

1. Cornell University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-8298

Reference17 articles.

1. Fehse,Wigbert,SolarAutonomousRendezvousandDockingofSpacecraft,UniversityofCambridge,Cambridge, UK, 2003.

2. Safe Trajectories for Autonomous Rendezvous of Spacecraft

3. Technology of Automated Rendezvous and Capture in Space

4. "OverviewoftheDARTMishapInvestigationResults,"Online,Internet.AccessedJan2010.Availableat< http://www.nasa.gov/pdf/148072main_DART_mishap_overview.pdf >

5. A Flux-Pinned Magnet-Superconductor Pair for Close-Proximity Station Keeping and Self-Assembly of Spacecraft

Cited by 13 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Experimental Evaluation for a Contactless Vibration Isolator Using the Flux Pinning Effect;Journal of Spacecraft and Rockets;2022-11

2. Using Small Satellites to Remove Non-Cooperative Space Debris;ASCEND 2022;2022-10-15

3. Flux Pinning Docking Interfaces in Satellites Using Superconducting Foams as Trapped Field Magnets;IEEE Transactions on Applied Superconductivity;2022-06

4. A Contactless Micro-Vibration Isolator Using the Flux Pinning Effect for Space Telescopes;Journal of Spacecraft and Rockets;2021-11-30

5. Flux-Pinned Dynamics Model Parameterization and Sensitivity Study;Journal of Aerospace Information Systems;2019-09