Journal of System Simulation ›› 2021, Vol. 33 ›› Issue (2): 434-444.doi: 10.16182/j.issn1004731x.joss.19-0507

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Simulation and Analysis for Gaussian Jitter Effects of Geosynchronous Satellite

Li Yulun1,2, Yang Wei1, Guo Jiayi1   

  1. 1. School of Electronics and Information Engineering, Beihang University, Beijing 100191, China;
    2. Key Laboratory of Electronics and Information Technology for Complex Aerospace System, National Space Science Center, Chinese Academy of Sciences, Beijing 101499, China
  • Received:2019-09-07 Revised:2019-12-31 Online:2021-02-18 Published:2021-02-20
  • Contact: Yang Wei (1983-), male, associate professor, research direction for moving target detection, space-borne SAR image formation, and 3D imaging. E-mail: yangweigigi@sina.com
  • About author:Li Yulun (1991-), male, engineer, doctoral candidate, research direction for complex system modeling and simulation and spatial-temporal signal processing. E-mail: yl_li@nssc.ac.cn
  • Supported by:
    National Natural Science Foundation of China (61701012)

Abstract: Ultrahigh-spatial-resolution and high-temporal-revisit appear to be realizable for future space-borne imaging missions. By taking advantage of satellites on the geosynchronous orbit, the wide-area continuous monitoring capacity to ground target zones becomes possible. Focus on the imaging target displacement, it is necessary to study the platform jitter during the conceptual modeling phase. Discrete Event System Specification (DEVS) is employed to abstract the observation area as an event generator. The attitude stabilization is digitalized and both theoretical analysis and simulation experiments of Gaussian-excited signals are provided. Simulation results show that the distributions of attitude responses preserve the normality. The offset distance of intersections between the optical axis and the ground could be more than ten kilometers, and the maximum estimation error of Doppler centroid frequencies is tens of Hertz. The conclusions help to improve the design accuracy of the geosynchronous satellite monitoring modeling.

Key words: attitude stabilization, DEVS-based modeling, micro-vibration, Doppler centroid

CLC Number: