Optics and Precision Engineering, Volume. 28, Issue 10, 2192(2020)
Design of attitude control system for ASRTU microsatellite
[1] [1] ZHANG H, YIN Y M, WANG X K. Study on the overseas microsatellite development status and product warranty[J]. Aerospace China, 2018(6): 51-54.(in Chinese)
ZHANG H, YIN Y M, WANG X K. Study on the overseas microsatellite development status and product warranty[J]. Aerospace China, 2018(6): 51-54.(in Chinese)
[2] [2] KOPACZ J R, HERSCHITZ R, RONEY J. Small satellites an overview and assessment[J]. Acta Astronautica, 2020, 170: 93-105.
KOPACZ J R, HERSCHITZ R, RONEY J. Small satellites an overview and assessment[J]. Acta Astronautica, 2020, 170: 93-105.
[3] [3] YAO Y SH. Research on Development Trend and Application of Modern Small Satellite Technology [J].Innovation Science and Technology,2019,(2): 158-159. (in Chinese)
YAO Y SH. Research on Development Trend and Application of Modern Small Satellite Technology [J].Innovation Science and Technology,2019,(2): 158-159. (in Chinese)
[4] [4] LIN L X. Micro satellite technology development and application prospects [J].Space International,2019,(6): 46-48. (in Chinese)
LIN L X. Micro satellite technology development and application prospects [J].Space International,2019,(6): 46-48. (in Chinese)
[5] [5] YOSHIDA K, YONETOKU D, ARIMOTO M, et al.. Kanazawa-SAT^3: micro-satellite mission for monitoring X-ray transients coincide with gravitational wave events[C].SPIE Astronomical Telescopes + Instrumentation. Proc SPIE 10699, Space Telescopes and Instrumentation 2018: Ultraviolet to Gamma Ray, Austin, Texas, USA. 2018, 1069: 1069962.
YOSHIDA K, YONETOKU D, ARIMOTO M, et al.. Kanazawa-SAT^3: micro-satellite mission for monitoring X-ray transients coincide with gravitational wave events[C].SPIE Astronomical Telescopes + Instrumentation. Proc SPIE 10699, Space Telescopes and Instrumentation 2018: Ultraviolet to Gamma Ray, Austin, Texas, USA. 2018, 1069: 1069962.
[6] [6] CAO M Y. Research on Magnetic Attitude Control Methods of Earth Observation Micro Satellite in Low Earth Orbit[D]. Harbin: Harbin Institute of Technology, 2017.(in Chinese)
CAO M Y. Research on Magnetic Attitude Control Methods of Earth Observation Micro Satellite in Low Earth Orbit[D]. Harbin: Harbin Institute of Technology, 2017.(in Chinese)
[7] [7] LI D, ZHU ZH C, ZHANG R, et al.. The design and in-orbit test of the companion microsatellite attitude control system in SZ-7 flight mission[J]. Journal of Astronautics, 2011, 32(3): 495-501.(in Chinese)
LI D, ZHU ZH C, ZHANG R, et al.. The design and in-orbit test of the companion microsatellite attitude control system in SZ-7 flight mission[J]. Journal of Astronautics, 2011, 32(3): 495-501.(in Chinese)
[8] [8] SAKAI S I, FUKUSHIMA Y, SAITO H. Design and on-orbit evaluation of magnetic attitude control system for the "REIMEI" microsatellite[C].2008 10th IEEE International Workshop on Advanced Motion Control. March 26-28, 2008, Trento, Italy. IEEE, 2008: 584-589.
SAKAI S I, FUKUSHIMA Y, SAITO H. Design and on-orbit evaluation of magnetic attitude control system for the "REIMEI" microsatellite[C].2008 10th IEEE International Workshop on Advanced Motion Control. March 26-28, 2008, Trento, Italy. IEEE, 2008: 584-589.
[9] [9] LIU SH W, WAN S, RONG J G. The analysis and simulation of aircraft space environment disturbance torque[J]. Aerospace Control, 2015, 33(2): 78-81, 92.(in Chinese)
LIU SH W, WAN S, RONG J G. The analysis and simulation of aircraft space environment disturbance torque[J]. Aerospace Control, 2015, 33(2): 78-81, 92.(in Chinese)
[10] [10] XU ZH Y, CHEN Y K, ZHANG Y C, et al.. Study on integrated electrical system design and attitude control of microsatellite LH-2[J]. Manned Spaceflight, 2020, 26(1): 88-93, 81.(in Chinese)
XU ZH Y, CHEN Y K, ZHANG Y C, et al.. Study on integrated electrical system design and attitude control of microsatellite LH-2[J]. Manned Spaceflight, 2020, 26(1): 88-93, 81.(in Chinese)
[11] [11] WANG Q, LI X H, HE G S, et al.. Spacecraft attitude determination algorithm and precision analysis based on EKF[J]. Computer Measurement & Control, 2018, 26(6): 155-159.(in Chinese)
WANG Q, LI X H, HE G S, et al.. Spacecraft attitude determination algorithm and precision analysis based on EKF[J]. Computer Measurement & Control, 2018, 26(6): 155-159.(in Chinese)
[12] [12] SONG L. Research on In-orbit Calibration Methods for Star Tracker-gyro Attitude Determination System[D]. Harbin: Harbin Institute of Technology, 2011.(in Chinese)
SONG L. Research on In-orbit Calibration Methods for Star Tracker-gyro Attitude Determination System[D]. Harbin: Harbin Institute of Technology, 2011.(in Chinese)
[13] [13] CHEN X Q, GENG Y H. On-orbit calibration algorithm for gyros/star sensor[J]. Journal of Harbin Institute of Technology, 2006, 38(8): 1369-1373.(in Chinese)
CHEN X Q, GENG Y H. On-orbit calibration algorithm for gyros/star sensor[J]. Journal of Harbin Institute of Technology, 2006, 38(8): 1369-1373.(in Chinese)
[14] [14] CHEN X Q, GENG Y H. On-orbit calibration algorithm with star sensors of gyros[J]. Systems Engineering and Electronics, 2005, 27(12): 2112-2116.(in Chinese)
CHEN X Q, GENG Y H. On-orbit calibration algorithm with star sensors of gyros[J]. Systems Engineering and Electronics, 2005, 27(12): 2112-2116.(in Chinese)
[15] [15] TAO Z Y. On-orbit calibration technology of attitude measurement instruments[D]. Harbin: Harbin Institute of Technology, 2014.(in Chinese)
TAO Z Y. On-orbit calibration technology of attitude measurement instruments[D]. Harbin: Harbin Institute of Technology, 2014.(in Chinese)
[16] [16] FAN W. Nano Satellite Attitude Estimation with Magnetometer and Photodiodes Measurements[C]. 28th China Control and Decision Conference. Yinchuan: Editorial Department of Control and Decision,2016: 1866-1870.
FAN W. Nano Satellite Attitude Estimation with Magnetometer and Photodiodes Measurements[C]. 28th China Control and Decision Conference. Yinchuan: Editorial Department of Control and Decision,2016: 1866-1870.
[17] [17] MA X Y. Study on the Attitude Control System of Satellite with Reaction Wheels and Magnetotors[D]. Harbin: Harbin Institute of Technology, 2013.(in Chinese)
MA X Y. Study on the Attitude Control System of Satellite with Reaction Wheels and Magnetotors[D]. Harbin: Harbin Institute of Technology, 2013.(in Chinese)
[18] [18] WANG X, ZHANG Y, YIN Y M, et al.. Analysis and thoughts on microsatellite standardization status[J]. Aerospace China, 2018(12): 36-40.(in Chinese)
WANG X, ZHANG Y, YIN Y M, et al.. Analysis and thoughts on microsatellite standardization status[J]. Aerospace China, 2018(12): 36-40.(in Chinese)
[19] [19] HE G S, LI X H, WANG Q, et al.. Simulation research on Attitude Control System for Modular Spacecraft[J]. Modern Electronics Technique, 2018, 41(18): 131-134.(in Chinese)
HE G S, LI X H, WANG Q, et al.. Simulation research on Attitude Control System for Modular Spacecraft[J]. Modern Electronics Technique, 2018, 41(18): 131-134.(in Chinese)
[20] [20] WANG ZH Y. Research on the Attitude Control System for Nano-satellites Based on Micro-Reaction Wheels Units[D]. Hangzhou: Zhejiang University, 2017.(in Chinese)
WANG ZH Y. Research on the Attitude Control System for Nano-satellites Based on Micro-Reaction Wheels Units[D]. Hangzhou: Zhejiang University, 2017.(in Chinese)
Get Citation
Copy Citation Text
WANG Feng, NIU Shi-bo, YUE Cheng-fei, WU Fan, CHEN Xue-qin. Design of attitude control system for ASRTU microsatellite[J]. Optics and Precision Engineering, 2020, 28(10): 2192
Category:
Received: Apr. 10, 2020
Accepted: --
Published Online: Nov. 25, 2020
The Author Email: