1) integrated translational and attitude control
姿轨联合控制
1.
This paper mainly contains two parts: The design of the fuel optimal guidance law for the powered descending phase while another part is the design of the integrated translational and attitude control law for the terminal landing phase.
主要分为两大部分:第一部分是动力下降段的燃料最优制导律的设计,第二部分是最终着陆段姿轨联合控制律的设计。
2) coupling control of attitude and orbit
姿—轨耦合控制
3) orbit and attitude control
轨道与姿态控制
1.
The system built a 3-D model of satellite by software LightWave, and developed a new orbit and attitude control module by the interface between STK and Matlab.
该仿真系统采用建模软件LightWave建立卫星三维模型,利用STK/Matlab模块提供的接口功能,开发新的轨道与姿态控制模块,为用户定制的轨道与姿态控制方案提供仿真、验证和演示。
4) 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) Attitude and Orbit Control
姿轨控
1.
Attitude and Orbit Control subsystem which is an important part of a satellite attitude control system is the core components to achieve high-performance attitude and orbit measurement and control.
姿轨控下位机作为卫星姿轨控分系统的重要组成部分,是卫星实现高性能姿轨测量和控制的核心部件。
6) orbital attitude control system
轨道姿态控制系统
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