TY - GEN
T1 - A High-Precision Analytical Solar Radiation Pressure Model for a GEO Large Antenna Satellite
AU - Wang, Shijie
AU - Sun, Minzhe
AU - Cheng, Wuyang
AU - Gao, Feng
AU - Li, Jiayang
AU - Ji, Yi
N1 - Publisher Copyright:
© 2024 IEEE.
PY - 2024
Y1 - 2024
N2 - Large space antenna satellites, as representative large space structures, exhibit complex dynamic characteristics under space environmental perturbations due to their unique configurations, affecting operational stability. To investigate the impact of solar radiation pressure perturbations, this study employs an advanced orbital prediction algorithm. Addressing the unique configurations and variable area-to-mass ratios of these satellites, an high-precision analytical solar radiation pressure model was proposed. This model optimizes the calculation of perturbation forces and accurately derives the relationship between area-to-mass ratio and solar incidence angle. Comparative simulations with a macro-model method verified the method's accuracy and effectiveness. The model also precisely calculates perturbation torque for complex antenna structures. This high-precision model enhances the understanding of large space antenna satellites' dynamics and provides critical support for orbit and attitude control.
AB - Large space antenna satellites, as representative large space structures, exhibit complex dynamic characteristics under space environmental perturbations due to their unique configurations, affecting operational stability. To investigate the impact of solar radiation pressure perturbations, this study employs an advanced orbital prediction algorithm. Addressing the unique configurations and variable area-to-mass ratios of these satellites, an high-precision analytical solar radiation pressure model was proposed. This model optimizes the calculation of perturbation forces and accurately derives the relationship between area-to-mass ratio and solar incidence angle. Comparative simulations with a macro-model method verified the method's accuracy and effectiveness. The model also precisely calculates perturbation torque for complex antenna structures. This high-precision model enhances the understanding of large space antenna satellites' dynamics and provides critical support for orbit and attitude control.
KW - large space antenna satellites
KW - orbital prediction algorithm modeling
KW - solar radiation pressure
KW - space environmental perturbations
UR - https://www.scopus.com/pages/publications/85207485517
U2 - 10.1109/EEI63073.2024.10696878
DO - 10.1109/EEI63073.2024.10696878
M3 - 会议稿件
AN - SCOPUS:85207485517
T3 - 2024 6th International Conference on Electronic Engineering and Informatics, EEI 2024
SP - 1837
EP - 1842
BT - 2024 6th International Conference on Electronic Engineering and Informatics, EEI 2024
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 6th International Conference on Electronic Engineering and Informatics, EEI 2024
Y2 - 28 June 2024 through 30 June 2024
ER -