1) Attitude and orbit control system
姿轨控系统
1.
Attitude and orbit control system simulation of satellite based on HLA/pRTIwere researched coming up with the basic frame of attitude and orbit control system simulation software platform.
基于高层系统结构HLA/pRTI对卫星姿轨控系统的仿真进行了初步研究,提出了姿轨控系统仿真软件平台的基本框架,介绍了姿轨控系统模型,给出了联邦FOM模型及时间管理策略。
2) Attitude and Orbital Control System
卫星姿轨控系统
3) Orbit & Attitude Control System
姿轨控制系统
1.
In this thesis, the qualitative-model-based fault diagnosis methods for Satellite Orbit & Attitude Control System are studied in order to provide ones with novel approaches to build the fault diagnosis system, which possesses good visualization and practicality.
本文主要研究基于定性模型的卫星姿轨控制系统的故障诊断方法,其目的是为建立具有可视化好,实用性强的卫星控制诊断系统提供新的技术途径,以克服定量模型计算复杂、不便应用的缺陷,克服传统的基于规则方法知识获取困难和灵活性差的缺点。
5) orbital attitude control system
轨道姿态控制系统
6) Attitude control system
姿控系统
1.
The schematic diagram of warhead attitude control system ground-test equipment is analyzed based on fault diagnosis,and the diagnostic information flow model(DIFM)of circuit is built.
从故障诊断的角度分析弹头姿控系统地测设备的原理,建立了电路的诊断信息流模型。
2.
Simulations run with a missile attitude control system proved the validity and feasibility of this new approach.
通过应用于某导弹姿控系统仿真计算证明了该方法的有效性与可行
3.
The application of gravity gradient in the attitude control system of mini-satellites provides an advantaged tool for the development and research of the miniaturization of satellites.
分析比较了目前卫星采用姿控的原理和方法,应用现代控制理论分析了重力梯度卫星姿控系统的性。
补充资料：美姿姿
1.同"美孜孜"。
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