Open Access
Issue |
JNWPU
Volume 37, Number 4, August 2019
|
|
---|---|---|
Page(s) | 673 - 681 | |
DOI | https://doi.org/10.1051/jnwpu/20193740673 | |
Published online | 23 September 2019 |
- Ma Yangming. The Design and Analysis on Vabration Isolation Efficiency of a Satellte Test System with Architecture of Disturbance Free Payload[D]. Habrbin, Harbin Institute of Technology, 2016 (In chinese) [Google Scholar]
- Zhang Wei, Zhao Yanbin, Liao He, et al. Design of Active-Quiet Isolated and Master-Slave Coordination Controlled Dual-Super Satellite Platform[J]. Aerospace Shanghai, 2014, 31(5): 7–11 [Article] (In chinese) [Google Scholar]
- Du Chao. Study on Dynamic Modeling and Controlling of a Satellite with a Architectrue of Disturbance Free Payload[D]. Harbin, Harbin Institute of Technology, 2015 (In chinese) [Google Scholar]
- Pedreiro N. Spacecraft Architecture for Disturbance Free Payload[J]. Journal of Guidance Control and Dynamics, 2002, 26(5): 794–804 [Article]">10.3969/j.issn.1006-1630.2014.05.002 [NASA ADS] [CrossRef] [Google Scholar]
- Pedreiro N, Carrier A, Lorell K, et al. Disturbance Free Payload Concept Demonstration[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit, Monterey, USA, 2002 [Article] [Google Scholar]
- Gonzales M, Pedreiro N, Brookes K, et al. Unprecedented Vibration Isolation Demonstration Using the Disturbance Free Payload Concept[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit, Providence, USA, 2004 [Article] [Google Scholar]
- Pedreiro N, Gonzales M, Foster B, et al. Agile Disturbance Free Payload[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit, San Francisco, USA, 2005 [Article] [Google Scholar]
- Huang Simeng. Research on Agile Technologies of Three-Rigid-Body Spacecraft Based on DFP System[D]. Harbin, Harbin Institute of Technology, 2016 (In chinese) [Google Scholar]
- Kong Xianren, Wu Chen, Liu Yuan, et al. Dynamic Modeling of Relative Motion for Disturbance-Free-Payload Spacecraft[J]. Journal of Astronautics, 2017, 38(11): 1139–1146 [Article] (In chinese) [Google Scholar]
- Zhang Dawei, Feng Xiaomei. The Technical Principle of Voice-Coil Actuator[J]. Journal of North University of China, 2006(3): 224–228 [Article] (In chinese) [Google Scholar]
- Liu Jian, Zhu Zhanxia, Ma Jiajin. Establishing Spacecraft's Relative Orbit and Attitude Coupling Dynamics Model Based on Screw Theory[J]. Journal of Northwestern Polytechnical University, 2013, 31(4): 590–595 [Article] (In chinese) [Google Scholar]
- Zhu Zhanxia, Ma Jiajin, Fan Ruishan. Coupling Analysis on Relative Motion of Spacecraft Attitude and Orbit Model Based on Dual Quaternion[J]. Journal of Northwestern Polytechnical University, 2015, 33(6): 887–891 [Article] (In chinese) [Google Scholar]
- Zhu Zhanxia, Ma Jiajin, Fan Ruishan. Synchronization Control of Relative Motion for Spacecraft with Screw Theory-Based Description[J]. Acta Aeronautical et Astronautica Sinica, 2016, 37(9): 2788–2798 [Article] (In chinese) [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.