Model predictive control of low earth orbiting spacecraft with magneto-torquers-Reference-Cited by-同舟云学术

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Model predictive control of low earth orbiting spacecraft with magneto-torquers

Published:2006-10 Issue: Volume: Page:
ISSN:
Container-title:2006 IEEE Conference on Computer Aided Control System Design, 2006 IEEE International Conference on Control Applications, 2006 IEEE International Symposium on Intelligent Control
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Author:

Wood Mark,Chen Wen-Hua,Fertin Denis

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx5/4768844/4776587/04777100.pdf?arnumber=4777100

Cited by 6 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. Pulse Width Modulation Method Applied to Nonlinear Model Predictive Control on an Under-actuated Small Satellite;AIAA Scitech 2021 Forum;2021-01-04

2. A survey on active magnetic attitude control algorithms for small satellites;Progress in Aerospace Sciences;2019-08

3. Field programmable gate array based predictive control system for spacecraft rendezvous in elliptical orbits;Optimal Control Applications and Methods;2014-03-27

4. Robust Magnetic Attitude Control of Satellites;IEEE/ASME Transactions on Mechatronics;2013-08

5. A Miniaturized Two Axis Sun Sensor for Attitude Control of Nano-Satellites;IEEE Sensors Journal;2010-10

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