舰船电子工程2024，Vol.44Issue(1)：116-119,4.DOI:10.3969/j.issn.1672-9730.2024.01.023
基于J2摄动项的Runge-Kutta、Hermite数值轨道预报方法
Research on Satellite Orbit Prediction by Runge-Kutta Based on J2 Perturbation Term and Hermit
摘要
Abstract
A deduction of coordinate transformation of satellite orbit based on its describe method,and the method are pro-grammed by Matlab and validated by other coordinate transformation software.Then numerical method(such as Runge_Kutta meth-od based on J2 perturbation term,Hermite method)of satellite orbit prediction are analyzed,their prediction performance are simu-lated and compared with the HPOP prediction result in STK.关键词
J2摄动项/卫星轨道/预报/性能仿真Key words
J2 perturbation term/satellite orbit/prediction/performance simulation分类
航空航天引用本文复制引用
张政超,朱峰,郭伟锋,周磊..基于J2摄动项的Runge-Kutta、Hermite数值轨道预报方法[J].舰船电子工程,2024,44(1):116-119,4.
