1) orbit determination
定轨
1.
Analysis of the Application of BRT and CEI in Tracking and Orbit Determination for Data Relay Satellites;
BRT和CEI技术用于数据中继卫星测定轨的分析比较
2.
Unscented Kalman filter with application to orbit determination based on space-borne GPS;
UKF算法在星载GPS低轨卫星定轨中的应用
3.
GPS orbit determination based on CORS station from state bureau of surveying and mapping
基于国家测绘局GPS连续运行参考站的定轨
2) Orbit determination
轨道确定
1.
Orbit Determination Method of the Station of Low Accuracy of Angle Data;
低测角精度下的轨道确定计算方法
2.
Precision Orbit Determination of Low-Earth Orbiters under Magnetic Storms;
磁暴下的LEO卫星精密轨道确定
3.
Space Target Orbit Determination Expert System;
空间目标轨道确定专家系统
3) given trace
给定轨迹
1.
Traditionally,the determination of the parameters of link-flying shear mechanism is based on given trace.
连杆类飞剪机的机构参数确定，普遍认为属于传统的给定轨迹的设计。
4) autonomous orbit determination
自主定轨
1.
SINS/GPS integrated navigation system for satellite autonomous orbit determination;
适于卫星自主定轨的SINS/GPS组合导航系统
2.
Autonomous Orbit Determination of Micro Satellite Constellations;
小卫星星座自主定轨的论证与仿真
3.
Research and Simulation on Autonomous Orbit Determination for Navigation Satellites;
导航卫星自主定轨研究及模拟结果
5) orbital stability
轨道稳定
1.
The abstract results of Grillakis are used directly and the orbital stability of solitary waves of compound KDVtype equation with nonlinear terms of any order is examined.
应用Grillakis提出的轨道稳定性理论,研究了广义组合KDV方程ut+aupux+bu2pux+δuxxx=0(a,b,δ,p=C,p>0)的轨道稳定性。
2.
Based on the abstract result about orbital stability of solitary waves of nonlinear Hamiltonian system,by datailed spectral analysis and computation,it is proved that the explicit peakons are orbitally stable.
研究广义Camassa-Holm方程孤立波解的轨道稳定性问题。
3.
In this paper, we first establish some abstact results on the orbital stability and orbital instability for some abstract complex Hamitonian systems.
本论文首先对抽象复哈密顿系统建立了孤立波解的轨道稳定性与不稳定性的抽象定理；在此基础上证明了一类非线性复合物质中两族显示孤立波解(分别是各向异性中的慢波族和各向同性中的孤立波族)在速度v的某个范围内是轨道不稳定的，从理论上验证了国外相关的数值计算结果及猜测；本文还证明了广义浅水波方程的一族不光滑孤立波解的轨道稳定性。
6) precise orbit determination
精密定轨
1.
Based on the precise orbit determination and the three days continual ranging observation of the GEO artificial satellite,the attainable precision in predicting and determining the orbit of the GEO artificial satellite is studied for the different arc-lengths observation data.
在精密定轨的基础上,结合某GEO(地球同步轨道)卫星连续3天的测距观测资料,研究了使用GEO卫星的不同弧长的观测资料进行定轨和轨道预报的精度。
补充资料：定轨
1.一定的法则。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条