1) Orbit Determination
动力法定轨
1.
An approximate covariance analysis for orbit determination of geostationary satellites was given using two-way range data with and without VLBI-augmented measurements.
利用一个针对GEO卫星的简化动力法定轨的协方差分析模型,研究了联合测距跟踪网和甚长基线干涉测量(VLBI)对定轨精度的改善情况。
2) Dynamic orbit determination
动力学定轨
1.
It studies the application of acceleration data as a substitutive method for non-conservative perturbation force to dynamic orbit determination.
在对空间飞行环境十分复杂的低轨卫星进行动力学定轨时,常规的摄动力模型化方法难以胜任厘米级精度的定轨任务。
3) dynamic orbit
动力法轨道
1.
The Earth gravity field recovery by use of Kaula linear perturbation method is studied from CHAMP kinematic orbits and dynamic orbits.
介绍了Kau la线性摄动方法的基本原理和算法,基于CHAMP几何法轨道和动力法轨道,给出了利用该方法恢复地球重力场模型的实现过程,分析了Kau la线性摄动方法在实际应用中需要注意的问题。
4) Dynamic orbit measurement
动力法测轨
5) reduced-dynamic orbit determination
简化动力学定轨
1.
The definition, characteristics and mathematical model of pseudo-stochastic pulses utilized in reduced-dynamic orbit determination are systematically analyzed.
研究了简化动力学定轨方法中伪随机脉冲的定义、特征及估计的数学模型。
6) kinematic/dynamic orbit determination
动态/动力组合定轨
补充资料：轨轨
1.依循轨迹。
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