1.
Design of Robust Guidance Law for SINS/GPS Guided Bomb
惯性/卫星制导炸弹鲁棒制导律设计
2.
Nonliearity compensation for pseudolite/INS integrated navigation
伪卫星/惯性组合导航的非线性补偿
3.
Study on Satellite_Borne GPS/SINS Deeply Integrated Technology;
星载卫星/惯性深层全组合导航技术研究
4.
Research on the Data Processing Method in Satellite/SINS Integrated Navigation
卫星/捷联惯性组合导航数据处理方法研究
5.
satellite-inertial guidance integrated positioning sy
卫星-惯导组合定位系统
6.
satellite-inertial guidance integrated positioning system
卫星惯导组合定位系统
7.
integrated navstar hybrid inertial
卫星导航与惯导的组合系统
8.
In-Orbit Identification of the Inertial Matrix of Zero Momentum Satellite
基于GTLS的零动量卫星惯量矩阵在轨辨识
9.
According to common international practice, commercial satellites can be launched only after both the satellite and the rocket have been insured.
按照国际惯例，商业卫星发射只有在星箭得到保险之后才能进行。
10.
launching of a trial meteorological satellite
发射试验性气象卫星
11.
This paper presents exploratory research on fighting forms of an anti-satellite satellite.
介绍了反卫星卫星攻击方式的探索性研究。
12.
It Mainly studies a series of technology problems to correct INS using GPS/ GLONASS Double Satellites Receive Equipment.
重点研究了用GPS/LONASS双卫星接收机校正惯导的一系列技术问题。
13.
Study on Quick Ascertaining Method of Optimal Single Star in Celestial-Inertial Integrated Guidance
单星星光/惯性复合制导最佳星快速确定方法研究
14.
satellite - to - satellite tracking
卫星－卫星跟踪技术
15.
low altitude satellite
低高度卫星低空卫星
16.
Influence of Satellite Vibration on the Performance of Inter-Satellite Optical CDMA Communication System
卫星振动对星间光码分多址系统性能的影响
17.
Study of geometric characteristics of inter-satellite links between LEO layer and MEO layer in LEO/MEO satellite constellation
双层卫星星座层间链路几何参数特性研究
18.
Study on the Reliability of Control and Processing System of Pico-satellite;
皮卫星星载控制处理系统的可靠性研究