首页> 外文会议>China satellite navigation conference >Chapter 5 Application of Thrust Force Model in GEO's Orbit Determination in Case of Maneuvers

【24h】

Chapter 5 Application of Thrust Force Model in GEO's Orbit Determination in Case of Maneuvers

机译：第五章推力模型在机动情况下GEO轨道确定中的应用

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

GEO satellites play a significant role in COMPASS satellite navigation system. The GEO's orbit must be maneuvered periodically for station-keeping. The method of the maneuvering orbit determination and prediction must be studied for advancing the COMPASS navigation system service precision. In the paper, the continuous constant thrust maneuver model is established. And based on the measurement from C transponder, the COMPASS-GEO orbit determination is analyzed with maneuver arc. It realized the continuous orbit determination and prediction crossing the orbit maneuver.

机译：GEO卫星在COMPASS卫星导航系统中起着重要作用。必须定期对GEO的轨道进行操纵以保持位置。为了提高COMPASS导航系统的服务精度，必须研究机动轨道的确定和预测方法。建立了连续恒推力机动模型。并基于C应答器的测量结果，利用机动弧对COMPASS-GEO轨道确定进行了分析。实现了跨越轨道机动的连续轨道确定与预测。

著录项

来源
《China satellite navigation conference》|2013年|55-66|共12页
会议地点
作者
Jun-Li Zhang; Hong-Xing Qiu; Yong Yang; Wen-Ge Guo;
展开▼
作者单位

展开▼
会议组织
原文格式 PDF
正文语种
中图分类
关键词
GEO; Maneuver; Orbit determination; Orbit prediction;

机译：GEO;演习;轨道确定;轨道预测;

相似文献

外文文献
中文文献
专利

1. Orbit determination and thrust force modeling for a maneuvered GEO satellite using two-way adaptive Kalman filtering [J] . XU TianHe, HE KaiFei, XU GuoChang 中国科学:物理学力学天文学（英文版） . 2012,第004期

机译：使用双向适应性卡尔曼滤波机械地理卫星轨道确定和推力模型
2. Beidou satellite maneuver thrust force estimation for precise orbit determination [J] . Qiao Jing, Chen Wu GPS Solutions . 2018,第2期

机译：精确轨道测定的北斗卫星操纵力估计
3. Orbit determination across unknown maneuvers using the essential Thrust-Fourier-Coefficients [J] . Ko Hyun Chul, Scheeres Daniel J. Acta astronautica . 2016,第JANaaFEBa期

机译：使用基本推力-傅立叶系数确定未知机动的轨道
4. Chapter 5 Application of Thrust Force Model in GEO's Orbit Determination in Case of Maneuvers [C] . Jun-Li Zhang, Hong-Xing Qiu, Yong Yang, China satellite navigation conference . 2013

机译：第5章推力模型在机械轨道测定中的应用
5. Orthogonal functions over the oceans and applications to the determination of orbit error, geoid and sea surface topography from satellite altimetry. [D] . Hwang, Cheinway. 1991

机译：海洋的正交函数及其在确定卫星高度计的轨道误差，大地水准面和海面地形方面的应用。
6. A Robust Method to Detect BeiDou Navigation Satellite System Orbit Maneuvering/Anomalies and Its Applications to Precise Orbit Determination [O] . Fei Ye, Yunbin Yuan, Bingfeng Tan, 2017

机译：北斗导航卫星系统轨道操纵/异常的稳健检测方法及其在精密定轨中的应用
7. Determination of Spacecraft's Orbit Parameters and Maneuver with Specified Time of Thrust Pulse Application [O] . Г.К. Боровин, М.В. Захваткин, В.А. Степаньянц, 2012

机译：具有指定推力脉冲应用时间的航天器的轨道参数和机动的确定
8. A STUDY OF VERY HIGH ALTITUDE MANEUVERS USING AERODYNAMIC FORCES, Volume II - On the Effects- of Aerodynamic Force and Continuous Thrust in Very High Altitude Maneuvers at Orbital Speeds [R] . Adolf Busemann, Robert Dudley Culp, Ching-Yew Yang 1974

机译：利用空气动力学研究非常高海拔地区的第二卷 - 论轨道速度超高空机动中气动力和连续推力的影响

Chapter 5 Application of Thrust Force Model in GEO's Orbit Determination in Case of Maneuvers

摘要

著录项

相似文献

相关主题

期刊订阅