| Citation: | WANG T，JIAO H C，LIU J，et al. Design of attitude control method for ultra-low-orbit satellite with pneumatic steering gear[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（3）：548-558 （in Chinese） doi: 10.13700/j.bh.1001-5965.2021.0265
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To meet the differentiated needs of the attitude control of ultra-low orbit satellites, this study investigates the attitude control strategy with the assistance of pneumatic steering gears. The layout of the gear is designed and its aerodynamic characteristics are analyzed under the thin atmosphere of the ultra-low orbit, with the theoretical aerodynamic force up to the order of 10−1 N, and the aerodynamic torque the order of 10−1 N·m. On this basis, an attitude control strategy assisted by pneumatic steering gears is designed. Simulation results show that when the
| [1] |
BACON A, OLIVIER B S. Bringing down the cost of earth observation[C]//Proceedings of the 12th Reinventing Space Conference. Berlin: Springer, 2017: 1-7.
|
| [2] |
ROBERT P C E, ROMANO F, HERDRICH G, et al. Keynote: Discoverer-making commercial satellite operations in very low earth orbit a reality[C]//70th International Astronautical Congress (IAC). Reston: AIAA, 2019: 21-25.
|
| [3] |
DE FLORIO S, D’AMICO S, RADICE G. Virtual formation method for precise autonomous absolute orbit control[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(2): 425-438. doi: 10.2514/1.61575
|
| [4] |
DE FLORIO S, D’AMICO S, RADICE G. Precise autonomous orbit control in low earth orbit[C]//Astrodynamics Specialist Conference. Reston: AIAA, 2012: 4811.
|
| [5] |
WERTZ J R, SHAO A, TAYLOR C, et al. Moderately elliptical very low orbits (MEVLOs) as a long-term solution to orbital debris[C]//26th Annual AIAA/USU Conference on Small Satelites. Reston: AIAA, 2012: SSC12-IV-6.
|
| [6] |
吴勤. 透视俄罗斯军用卫星发展现状[J]. 太空探索, 2008(12): 46-49.
WU Q. Perspective of Russian military satellite development status[J]. Space Exploration, 2008(12): 46-49(in Chinese).
|
| [7] |
曾其鋆. 气动力矩在超低轨道卫星姿态控制方面的应用研究[D]. 哈尔滨: 哈尔滨工业大学, 2009: 41-56.
ZENG Q J. Applications of aerodynamic torque to ultra-low-orbit satellite attitude control[D]. Harbin: Harbin Institute of Technology, 2009: 41-56(in Chinese).
|
| [8] |
田春华, 马广富, 李传江, 等. 三轴稳定卫星姿态控制系统的一般性问题[J]. 自动化技术与应用, 2001(1): 9-12.
TIAN C H, MA G F, LI C J, et al. General problems of satellite attitude control[J]. Techniques of Automation and Applications, 2001(1): 9-12(in Chinese).
|
| [9] |
黄静. 三轴稳定航天器姿态最优控制方法研究[D]. 哈尔滨: 哈尔滨工业大学, 2010: 75-78.
HUANG J. Optimal attitude control for three-axis stabilized spacecrafts[D]. Harbin: Harbin Institute of Technology, 2010: 75-78(in Chinese).
|
| [10] |
段广仁, 钟震, 姜苍华. 航天器的一种无源自适应姿态控制方法[J]. 哈尔滨工业大学学报, 2011, 43(5): 1-7. doi: 10.11918/j.issn.0367-6234.2011.05.001
DUAN G R, ZHONG Z, JIANG C H. One scheme of passive adaptive attitude control for spacecraft[J]. Journal of Harbin Institute of Technology, 2011, 43(5): 1-7(in Chinese). doi: 10.11918/j.issn.0367-6234.2011.05.001
|
| [11] |
邵汉斌. 基于滑模控制的超低轨道航天器姿态控制方法研究[D]. 长沙: 国防科学技术大学, 2014: 12-16.
SHAO H B. Ultra-low-orbit spacecraft attitude control based on sliding mode control[D]. Changsha: National University of Defense Technology, 2014: 12-16(in Chinese).
|
| [12] |
KUMAR R R, MAZANEK D D, HECK M L. Simulation and Shuttle Hitchhiker validation of passive satellite aerostabilization[J]. Journal of Spacecraft and Rockets, 1995, 32(5): 806-811.
|
| [13] |
KUMAR R R, MAZANEK D D, HECK M L. Parametric and classical resonance in passive satellite aerostabilization[J]. Journal of Spacecraft and Rockets, 1996, 33(2): 228-234. doi: 10.2514/3.26745
|
| [14] |
PSIAKI M L. Spacecraft attitude stabilization using passive aerodynamics and acting magnetic torquing: AIAA-2003-5420[R]. Reston: AIAA, 2003.
|
| [15] |
PSIAKI M L. Magnetic torquer attitude control via asymptotic periodic linear quadratic regulation[J]. Journal of Guidance, Control, and Dynamics, 2001, 24(2): 386-394. doi: 10.2514/2.4723
|
| [16] |
GUETTLER D B. Satellite attitude control using atmospheric drag [D]. Dayton: Air Force Institute of Technology, 2007: 23-33.
|
| [17] |
刘辉, 伍斯宾斯基. 利用喷气装置卸载航天器积累角动量的最小工质损耗控制[J]. 航天控制, 2004, 22(5): 32-35. doi: 10.3969/j.issn.1006-3242.2004.05.008
LIU H, USPENSKY V B. Minimize propellant consumption during gyro system unloading process of spacecraft[J]. Aerospace Control, 2004, 22(5): 32-35(in Chinese). doi: 10.3969/j.issn.1006-3242.2004.05.008
|
| [18] |
张利宾. 基于磁控和轮控的微小卫星姿态控制算法研究[D]. 哈尔滨: 哈尔滨工业大学, 2007: 26-51.
ZHANG L B. Study on attitude control algorithm for micro-satellite using magnetotorquers and reaction wheels[D]. Harbin: Harbin Institute of Technology, 2007: 26-51(in Chinese).
|
| [19] |
李太玉, 张育林. 基于能量最优解析解的飞轮磁卸载方法[J]. 上海航天, 2006, 23(6): 1-9. doi: 10.19328/j.cnki.1006-1630.2006.06.001
LI T Y, ZHANG Y L. Momentum magnetic unloading basing on analytic equation of energy optimization[J]. Aerospace Shanghai, 2006, 23(6): 1-9(in Chinese). doi: 10.19328/j.cnki.1006-1630.2006.06.001
|
| [20] |
STEIGER C, ROMANAZZO M, EMANUELLI P P. The deorbiting of ESA’s gravity mission GOCE–Spacecraft operations in extreme drag conditions[C]//International Conference on Space Operations. Reston: AIAA, 2014: 1934.
|
| [21] |
何慧东. 日本“超低轨道技术试验卫星”任务及应用[J]. 国际太空, 2018(9): 50-53. doi: 10.3969/j.issn.1009-2366.2018.09.010
HE H D. Japan’s super low altitude test satellite mission and application[J]. Space International, 2018(9): 50-53(in Chinese). doi: 10.3969/j.issn.1009-2366.2018.09.010
|
| [22] |
温生林. 超低轨道卫星动力学建模与控制方法研究[D]. 长沙: 国防科学技术大学, 2016: 20-35.
WEN S L. Dynamic modeling and flight control for super low altitude satellite[D]. Changsha: National University of Defense Technology, 2016: 20-35(in Chinese).
|
| [23] |
周伟勇, 张育林, 刘昆. 超低轨航天器气动力分析与减阻设计[J]. 宇航学报, 2010, 31(2): 342-348. doi: 10.3873/j.issn.1000-1328.2010.02.007
ZHOU W Y, ZHANG Y L, LIU K. Aerodynamics analysis and reduced drag design for the lower LEO spacecraft[J]. Journal of Astronautics, 2010, 31(2): 342-348(in Chinese). doi: 10.3873/j.issn.1000-1328.2010.02.007
|
| [24] |
胡凌云, 张立华, 程晓丽, 等. 超低轨航天器气动设计与计算方法探讨[J]. 航天器工程, 2016, 25(1): 10-18. doi: 10.3969/j.issn.1673-8748.2016.01.002
HU L Y, ZHANG L H, CHENG X L, et al. Method of aerodynamic design and calculation for ultra-LEO spacecraft[J]. Spacecraft Engineering, 2016, 25(1): 10-18(in Chinese). doi: 10.3969/j.issn.1673-8748.2016.01.002
|
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