1) relative orbital parameter
相对轨道参数
2) relative orbital element method
相对轨道根数法
3) Relative orbit elements
相对轨道根数
1.
Formulations of the relative motion on highly elliptic orbits are developed by kinematic method which takes the relative orbit elements as the variable,and then the precision of the formation is analyzed.
完善了以相对轨道根数为变量的大椭圆编队相对运动模型,分析了模型的误差。
5) orbital elements
轨道参数
1.
GPS signal simulator simulates the satellite signals obtained by GPS,and the six orbital elements of GPS satellite are important parameters in GPS signal simulator.
GPS信号模拟器模拟产生GPS接收机前端接收到的卫星信号,其中需要确定的关键参数是GPS卫星的6个轨道参数。
2.
Based on the examples analyzed,this paper mainly discusses the impacts of the polynomial degree,fit time span and interval of the fitting points when using chebyshev polynomial to fit the satellite orbit,the situation using more orbital elements and the area and choosing of the orbital elements are also discussed at last.
以实例分析为基础,主要讨论了利用切比雪夫多项式拟合GPS卫星轨道时多项式阶数、时段长度、拟合点间隔等因素的设置问题;并对使用多组轨道参数进行轨道拟合的情况进行了分析;最后讨论了轨道参数的使用范围和选择问题;得出了有用的结论。
6) orbit parameter
轨道参数
1.
The model of the space missile intercepting quickly was built and the orbit parameters were solved based on the theories of the orbit dynamics,second time and energies optimization,respectively.
根据轨道动力学的理论,建立空间导弹快速拦截模型,求解轨道参数。
2.
Using this estimator, we obtain the high accurate estimator of the orbit parameters of long range rocket and the system errors of guidance instrument and orbit tracking.
利用了该估计，得到了远程火箭的轨道参数、制导工具系统误差和外弹系统误差的高精度估计。
补充资料：轨道保持(见航天器轨道控制)
轨道保持(见航天器轨道控制)
orbit keeping
guidQo baoehi轨道保持(o rbit keePing)见航天器轨道控制。
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