Citation: | CHEN Gaojie, CHANG Lin, LI Jing, YANG Xiubin, YANG Chunlei, LI Yanbo. Configuration Keeping Control of Stereo Imaging with Dual-satellite Following Flying Formation[J]. Chinese Journal of Space Science, 2021, 41(6): 954-961. doi: 10.11728/cjss2021.06.954 |
[1] |
LIN Laixing, ZHANG Xiaolin. Current status and developing trends of nanosatellites formation flying[J]. Spacecraft Eng., 2017, 26(5):65-73(林来兴, 张小琳. 纳型卫星编队飞行技术现状及发展趋势[J]. 航天器工程, 2017, 26(5):65-73)
|
[2] |
LIU GuoPing, ZHANG Shijie. A survey on formation control of small satellites[J]. Proc. IEEE, 2018, 106(3):440
|
[3] |
SUN Jun, HUANG Jing, ZHANG Xianliang, et al. Dynamics and control of spacecraft formation flying in Earth orbit[J]. Mech. Eng., 2019, 41(2):117-136(孙俊, 黄静, 张宪亮, 等. 地球轨道航天器编队飞行动力学与控制研究综述[J]. 力学与实践, 2019, 41(2):117-136)
|
[4] |
SAPTARSHI Bandyopadhyay, GIRI P S, REBECCA Foust, et al. A review of impending small satellite formation flying missions[C]//53rd AIAA Aerospace Sciences Meeting. Kissimmee:AIAA, 2015:1-17
|
[5] |
ZHANG Renwei. Dynamics and Control of Satellite Orbit Attitude[M]. Beijing:Beijing University of Aeronautics and Astronautics Press, 1998(章仁为. 卫星轨道姿态动力学与控制[M]. 北京:北京航空航天大学出版社, 1998)
|
[6] |
LI Liang, WANG Hong, LIU Liangyu, et al. Development of micro-satellite constellation and formation technologies[J]. Space Elect. Technol., 2017, 14(1):13-14(李亮, 王洪, 刘良玉, 等. 微小卫星星座与编队技术发展[J]. 空间电子技术, 2017, 14(1):13-14)
|
[7] |
KE Z, ZHENQI H, MEIBO L. Study on maintaining formations during satellite formation flying based on SDRE and LQR[J]. Open Phys., 2017, 15(1):394-399
|
[8] |
WANG Yuedong. Research on Two-satellite Formation Control Based on Lyapunov Function[D]. Taiyuan:North University of China, 2017(王月东. 基于李雅普诺夫函数的双星编队控制研究[D]. 太原:中北大学, 2017)
|
[9] |
XING Jianjun, YU Yang, WANG Yi, et al. Robust control of low earth orbit satellites formation based on improved linear quadratic regulator[J]. J. Natl. Defense Univ. Sci. Technol., 2016, 38(3):100-106(杏建军, 于洋, 王祎, 等. 基于改进线性二次型调节器的近地轨道编队卫星鲁棒控制[J]. 国防科技大学学报, 2016, 38(3):100-106)
|
[10] |
LEE D. Nonlinear disturbance observer-based robust control for spacecraft formation flying[J]. Aerosp. Sci. Technol., 2018, 76:1-9
|
[11] |
WANG Youliang, ZHENG Jianhua, LI Mingtao. Analytical formation keeping control strategy for micro-satellites[J]. Space Sci., 2018, 38(6):925-933(王有亮, 郑建华, 李明涛. 微小卫星编队飞行解析构型维持控制方法[J]. 空间科学学报, 2018, 38(6):925-933)
|
[12] |
STARIN S R, YEDAVALLI R K, SPARKS A G. Design of a LQR controller of reduced inputs for multiple spacecraft formation flying[C]//American Control Conference. Arlington:IEEE, 2001:1327-1332
|
[13] |
CUI Wenhao. Research on the Satellite Formation Reconfiguration and Keeping under J2 Perturbation[D]. Harbin:Harbin Engineering University, 2019
|
[14] |
LEE D. Nonlinear disturbance observer-based robust control for spacecraft formation flying[J]. Aerosp. Sci. Technol., 2018, 76:82-90
|
[15] |
YAO Junyu. Finite-time Attitude Control for Tethered Satellite System in Deep Space[D]. Harbin:Harbin Institute of Technology, 2016
|
[16] |
HU Q L, NIU G L, WANG C L. Spacecraft attitude fault-tolerant control based on iterative learning observer and control allocation[J]. Aerosp. Sci. Technol., 2018, 75:245-253
|
[17] |
SHI K K, LIU C, BIGGS J D, et al. Observer-based control for spacecraft electromagnetic docking[J]. Aerosp. Sci. Technol., 2020, 99:105759
|
[18] |
ZHANG Ke, COCQUEMPOT Vincent, JIANG Bin. Adjustable parameter-based multi-objective fault estimation observer design for Continuous-Time/Discrete-Time dynamic systems[J]. Int. J. Control Automat. Syst., 2017, 15(3):1077-1088
|
[19] |
ZHANG Siying, GAO Liqun. Modern Control Theory[M]. Beijing:Tsinghua University Press, 2017
|
[20] |
MARCELO Dias Pedroso, CLAUDINOR Bitencourt Nascimento, ANGELO Marcelo Tusset, et al. A hyperbolic tangent adaptive PID+ LQR control applied to a step-down converter using poles placement design implemented in fpga[J]. Math. Probl. Eng., 2013, 2013(13):1
|