Study on Simulation Technology of Agile Satellite Working Mode Based on MVC

doi:10.16182/j.issn1004731x.joss.201703010

Journal of System Simulation ›› 2017, Vol. 29 ›› Issue (3): 537-545.doi: 10.16182/j.issn1004731x.joss.201703010

Previous Articles Next Articles

Study on Simulation Technology of Agile Satellite Working Mode Based on MVC

Zhao Lin, Yang Huizhi, Hao Yong^*, Liu Yuan, Wu Xiaowen

Automation Institute of Harbin Engineering University, Harbin 150001, China

Received:2015-05-28 Revised:2015-07-28 Online:2017-03-08 Published:2020-06-02

Abstract

Abstract: To study on the method and effectiveness of large angle maneuver and push broom imaging for agile satellite, an agile satellite working mode simulation system was established based on MVC though analyzing imaging model, satellite parameters and orbital parameters of “Quickbird2”, a high resolution of commercial remote sensing satellite in the United States. The simulation system took VC2010 as software development environment, adopted MVC framework technology to realize information exchange between various members of the system, put satellite orbit data, attitude data and imaging data of simulation output into STK engine to realize 2D/3D scene visualization of agile satellite attitude switching and push broom imaging, the process data of simulation were stored in database for post analysis. The simulation results show that the simulation system realizes the interactive analysis of the working mode and the effectiveness of agile satellite, and can provide support for the overall design of the agile satellite.

Key words: agile satellite, push broom imaging, MVC, STK

CLC Number:

U283.1

Zhao Lin, Yang Huizhi, Hao Yong, Liu Yuan, Wu Xiaowen. Study on Simulation Technology of Agile Satellite Working Mode Based on MVC[J]. Journal of System Simulation, 2017, 29(3): 537-545.

References

[1] Michel Lemaitre, Gerard Verfaillie.Selecting and scheduling observations of agile satellites[J]. Aerospace Science and Technology (S1270-9638), 2002, 6(5): 367-381.
[2] Lappas V J, Steyn W H, Underwood C.Design and testing of a control moment gyroscope cluster for small satellites[J]. Journal of Spacecraft and Rockets (S0022-4650), 2005, 42(4): 729-739.
[3] 郑立君. 挠性卫星姿态大角度机动路径的设计与优化 [D]. 南京: 南京理工大学, 2012.
(Zheng Lijun.Design and Optimization of Attitude Large Angle Maneuvering Path for Flexible Satellite [D]. Nanjing, China: Nanjing University of Science and Technology, 2012.)
[4] Wertz. Spacecraft Attitude Determination and Control[C]// Guidance, Navigation, and Control Conference, vol. AIAA-2007-6734. USA: AIAA, 1970: 211-245.
[5] 屠善澄. 卫星姿态动力学与控制(2) [M]. 北京: 中国宇航出版社, 2003.
(Tu Shancheng.Satellite Attitude Dynamics and Control(2) [M]. Beijing, China: China Aerospace Press, 2003.)
[6] 叶东. 敏捷卫星姿态快速机动与稳定控制方法研究 [D]. 哈尔滨: 哈尔滨工业大学, 2013.
(Ye Dong.Research on Fast Maneuver and Stabilization Control for Agile Satellite [D]. Harbin, China: Harbin Institute of Technology, 2013.)
[7] Yao Zhang, Jingrui Zhang.Combined control of fast attitude maneuver and stabilization for large complex spacecraft[J]. Acta Mechanica Sinia, 2013, 29(6): 875-882.
[8] Abdollahi Abbas, Dastranj Mohamad Reza.Satellite Attitude Tracking for Earth Pushbroom Im-aginary with Forward Motion Compensation[J]. International Journal of Control and Automation (S2005-4297), 2014, 7(1): 437-446.
[9] Takada K, Kojima H, Matsuda N.Control moment gyro singularity-avoidance steering control b-ased on singular-surface cost function[J]. Journal of guidance, control, and dynamics (S0731-5090), 2010, 33(5): 1442-1450.
[10] Kang G, Xiaojing D, Xinyuan M.Research on Mu-lti update rate Method of Precise Satellite A-ttitude Determination Based on Gyro and Star-Sensor[J]. AIAA, Guidance, Navigation, and Control Conference (S0001-1452), 2011, 163(1):149-154.

Study on Simulation Technology of Agile Satellite Working Mode Based on MVC

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 2

Recommended Articles

Metrics

Comments

[1]	He Miao, Wang Hao, Huang Yong, Xue Shao, Shen Yinqing. Design of Fragment Warhead Simulation System Based on MVC Distributed Framework [J]. Journal of System Simulation, 2020, 32(9): 1744-1752.
[2]	Zhang Cuicui, Zhou Guoxiang, Yu Lei, Shi Lei, Wang Qingqing. Research on the MVC-based Generation of Test Paper and the Algorithm of Subjective Criterion [J]. Journal of System Simulation, 2020, 32(1): 105-112.