EDP Sciences logo
Submit your paper
Search
Menu
All issues Volume 36 / No 1 (February 2018) JNWPU, 36 1 (2018) 1-6 References
Open Access
Issue
JNWPU
Volume 36, Number 1, February 2018
Page(s) 1 - 6
DOI https://doi.org/10.1051/jnwpu/20183610001
Published online 18 May 2018
  1. Twiggs R. Small Satellites:Past, Present, and Future[M]. Segundo, California, the Aerospace Press, 2008: 151-157 [Google Scholar]
  2. Fish C S, Swenson C M, Crowley G, et al. Design, Development, Implementation, and On-Orbit Performance of the Dynamic Ionosphere CubeSat Experiment Mission[J]. Space Science Reviews, 2014, 181(4):61-120 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  3. Yu Xiaozhou, Zhou Jun, Zhu Linyu. Life Time Analysis of Chinese Aoxiang-1 CubeSat of Lower Thermosphere Research[J]. Journal of Northwestern Polytechnical University, 2013, 31(6): 896-900 (in Chinese) [Article] [Google Scholar]
  4. Si J T, Gao Y, Abadi C, Slew Control of Prolate Spinners Using Single Magnetorquer[J]. Journal of Guidance Control and Dynamics, 2016, 39(3) : 715-723 [Article] [NASA ADS] [Google Scholar]
  5. Anton H J R. Magnetic Control of Dual-Spin and Bias-Momentum Spacecraft[J]. Journal of Guidance Control and Dynamics, 2012, 35(4) : 1158-1168 10.2514/1.55869 [CrossRef] [Google Scholar]
  6. Nobuo S, Toshinori K, Kazuya Y. Attitude Determination and Control System for Nadir Pointing Using Magnetorquer and Magnetometer[C]//2016 IEEE Aerospace Conference, Big Sky, MT, USA, 2016: 1-15[Article] [Google Scholar]
  7. Mohamad F M, Mehran M. Design of Manufacturing of a Research Magnetic Torquer Rod[J]. Contemporary Engineering Science, 2010, 3(5) : 227-236 [Article] [Google Scholar]
  8. Degrandi R H, Heroe W, Budi S, et al. Design of Attitude Determination and Control System Using Microstrip Magnetorquer for Nanosatellite[C]//2016 International Conference on Control, Electronics, Renewable Energy and Communications, Bandung, Indonesia, 2016: 65-69 [Google Scholar]
  9. Koudelka O, Egger G, Josseck B, et al. TUGSAT-1/BRITE-Austria——The first Austrian Nanosatellite[J]. Acta Astronautica, 2009, 64(11) : 1144-1149 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  10. Bouwmeester J, Reijneveld J, Hoevenaars T, et al. Design and Verification of a very Compact and Versatile Attitude Determination and Control System for the Delfi-N3XT Nanosatellite[C]//2012 Small Satellites Systems and Services, Portorož, Slovenia, 2012: 1-5 [Google Scholar]
  11. Zhang Lingyun, Guo Lei, Yang Zhaohua. Design and Implementation of the Air Core Magnetic Torquer for Micro/Nano Satellite[C]//Proceedings of the Fifth Annual Conference of China Aerospace Society Deep Space Exploration Technology Specialized Committee, Changsha, 2008: 34-37(in Chinese) [Google Scholar]
  12. Feng Q, Liu Y, Li L, et al. Optimal Design and Implementation of Coreless Magnetic Torque for Nano-Satellites[C]//Proceedings of the 32nd Chinese Control Conference, Xi'an, 2013: 5609-5613 [Article] [Google Scholar]

Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.

Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.

Initial download of the metrics may take a while.