Advanced Search
Volume 31 Issue 06
Jun.  2005
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2005  >  31(06): 668-672.
HUANG Jun, HUAI Jin-peng, WU Zheet al. Optimization Selection in Conceptual Design of Advanced Trainer Aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(6): 656-659. (in Chinese)
Citation: Tang Liang, Xu Shijie. Integrated power and attitude control system based on VSCMGs for agile small satellite[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(06): 668-672. (in Chinese)
shu

Integrated power and attitude control system based on VSCMGs for agile small satellite

  • School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • Received Date: 25 Apr 2004
  • Publish Date: 30 Jun 2005
    Abstract
  • The multi-projects attitude maneuver problem for ASSAT(agile small satellite) with VSCMGs(variable speed control moment gyros) as actuator was investigated. Under some limits, such as, the saturation of actuators, the requirement of attitude maneuver, the measurement and tracking ability of sensors, a nonlinearly integrating power and attitude controller was designed. The quaternion drift resulting from frequent maneuver was tuned. A VSCMGs steering law was provided. According to the singularity indicator of configuration, the steering tasks including singularity avoidance and wheel speed equalization were assigned soundly. Two corresponding methods were designed. The law was switched form one method to another if the indicator reached the defined condition. A numerical example for the IPACS(integrated power and attitude control system) with VSCMGs of pyramid configuration was given. The simulating results show that the ASSAT is able to satisfy simultaneously the requirements of the rapid speed attitude maneuver and stability, as well as the energy control and wheel speed equalization.

     

    • FullText(HTML)
    • References(1)
  • [1] Bong W, David B, Christopher H. Rapid multi-target acquisition and pointing control of agile spacecraft . AIAA-2000-4546, 2000 [2] Lappas V J, Steyn W H, Underwood C I. Practical results on the development of a control moment gyro based attitude control system for agile small satellites . In:Logan. The Sixteenth Annual AIAA/USU Conference on Small Setellites . Utah:AIAA, 2002. 12~15 [3] Schaub H, Vadali S R, Junkins J L. Feedback control law for variable speed control moment gyros[J]. The Journal of Astronautical Sciences, 1998, 46(3):307~328 [4] Schaub H, Junkins J L. Singularity avoidance using null motion and variable-speed control moment gyros[J]. Journal of Guidance Control and Dynamics, 2000, 23(1):11~16 [5] Richie D J, Tsiotras P, Fausz J L. Simultaneous attitude control and energy storage using VSCMGs:theory and simulation . In:Bruce H Krogh. Proceedings of the American Control Conference . Virginia:Omnipress, 2001.3973~3979 [6] 贾英宏,徐世杰.采用变速控制力矩陀螺的一种姿态/能量一体化控制研究 .宇航学报, 2003, 24(1):32~37 Jia Yinghong, Xu Shijie. Study on integrated attitude/power control using variable speed control moment gyros[J]. Journal of Astronautics, 2003, 24(1):32~37(in Chinese)
    • Relative Articles

  • Relative Articles

    [1]MA J L，LIU Y H，MA Z P，et al. Lightweight lip reading method based on decoupling homogeneous self-knowledge distillation[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（12）：3709-3719 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0931.
    [2]WANG X L，YIN H，HE M. Potential conflict prediction of mobile targets in airfield areas based on LSTM[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（6）：1850-1860 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0505.
    [3]LI Bowen, LEI Xiaoyong. Flight task recognition and action segmentation based on SVM[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0635
    [4]WANG Luofeng, CHEN Renliang, ZHAO Yu. Fuzzy anti-swing controller for improving handling quality of helicopter slung load operation[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0265
    [5]LYU Yuzhu. Study on Flight Characteristics and Speed Limit of Helicopter with Slung Load[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0563
    [6]TAN J F，YANG Y X，ZHANG W G，et al. Influence of crosswind on helicopter brownout[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（10）：3111-3122 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0794.
    [7]ZHEN X D，WANG Z A，HU R C，et al. Aircraft flight qualities of short take-off and vertical landing[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1576-1585 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0413.
    [8]WANG R P，SONG X，CHEN K，et al. Pedestrian trajectory prediction method based on pedestrian pose[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1743-1754 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0557.
    [9]YANG K L，HAN D. Influence of rotor/wing aerodynamic interference on performance of compound helicopters[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1761-1771 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0561.
    [10]DUAN B，YANG S，LI A J. Design of LPV control law for unmanned helicopter[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（4）：879-890 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0340.
    [11]FENG W C，ZHANG T，LI W. Experimental study on adverse attitude emergency evacuation of civil aircraft after crash landing[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1553-1562 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0483.
    [12]ZHANG X C，WAN Z Q，YAN D. Optimal active twist control for rotor vibration reduction[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3397-3408 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0105.
    [13]SONG Z R，ZHAO J C，YANG W F. Boundary protection control method of helicopter power system based on flight test analysis[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（1）：100-105 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0431.
    [14]DENG B H，XU J F. Active disturbance rejection control of attitude of compound unmanned helicopter[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：3100-3107 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0788.
    [15]TAN J F，HAN S，WANG C，et al. Accelerated computational method of helicopter brownout based on DEM[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（6）：1352-1361 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0450.
    [16]JIN Z B，LI D C，SUN Y，et al. Man-machine cooperative control of helicopter and flight experimental validation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：3022-3030 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0038.
    [17]LIN Miao, MENG Gang, JU Yongjian, XU Weisheng, CAO Yi. Design and optimization of large-stroke decoupled three-translational micro-positioning platform[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(7): 1252-1262. doi: 10.13700/j.bh.1001-5965.2021.0007
    [18]WANG Shaoping, CHEN Rentong, ZHANG Chao. Reliability estimation for aircraft hydraulic pump based on bivariate performance degradation analysis[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(9): 1613-1623. doi: 10.13700/j.bh.1001-5965.2022.0297
    [19]YANG Shang-hang, XU Guo-ning, JIA Zhong-zhen, LI Yong-xiang, ZHUANG Chun-yu, YANG Yan-chu. Research on wireless charging coil location method of aircraft based on machine learning[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023-0006
    [20]YIN Zengyuan, CAI Yuanwen, REN Yuan, WANG Weijie, CHEN Xiaocen, YU Chunmiao. Decoupled active disturbance rejection control method for magnetically suspended rotor based on state feedback[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(7): 1210-1221. doi: 10.13700/j.bh.1001-5965.2021.0021
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(2729) PDF downloads(254) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return