航空宇航科学与技术的英文

• aeronautical and astronautical science and technology

• "航空"英文翻译    aviation; voyage
• "宇航"英文翻译    astronavigation; space navig ...
• "科学"英文翻译    science; scientific knowledg ...
• "与"英文翻译    take part in; participate in
• "技术"英文翻译    technology; skill; technique ...
• "科学与技术" 英文翻译 :    sc & t; science & techology; science and technology; sciences et techniques
• "technology]科学与技术" 英文翻译 :    sc & t
• "核科学与技术" 英文翻译 :    nuclear science and technology
• "坏科学与技术" 英文翻译 :    mechanical science and technology
• "科学与技术局" 英文翻译 :    dsto; office of science and technology
• "膜科学与技术" 英文翻译 :    membrane science and technology
• "热科学与技术" 英文翻译 :    journal of thermal science and technology
• "宇航科学进展" 英文翻译 :    progress in aerospace science
• "包装科学与技术" 英文翻译 :    packaging materials; packaging science and technology
• "兵器科学与技术" 英文翻译 :    armament science and technology
• "测绘科学与技术" 英文翻译 :    surveying and mapping
• "电子科学与技术" 英文翻译 :    electronic science and technology; electronics science and technology
• "防火科学与技术" 英文翻译 :    fire prevention science and technology
• "纺织科学与技术" 英文翻译 :    textile science and techniques
• "光信息科学与技术" 英文翻译 :    optic information science & technology; optical information science and technology
• "焊接科学与技术" 英文翻译 :    science and technology of welding and joining
• "环境科学与技术" 英文翻译 :    environmental science technology
• "计算机科学与技术" 英文翻译 :    journal of computer science and technology
• "建造科学与技术所" 英文翻译 :    institute of construction science and techniques
• "科学与技术总署" 英文翻译 :    office of science and technology

• Aeronautical and astronautical science and technology
  航空宇航科学与技术
• Based on chinese tracking and data relay satellite ( ctdrs ) in the future , the antenna pointing control and complex control theory of user satellite are studied deeply in this dissertation , which is funded by the improve item of dept . of astronautic engineering and mechanics ? “ the teaching demonstration of antenna pointing control system in tdrss ” . the main contents of this dissertation are consisted of the following parts : firstly , dynamics equation is derived using lagrange equation for user satellite , so as the kinetics equations of user satellite at the same time are expressed in the form with matrix differential equations that is suitable for attitude control system design and analysis
  本学位论文结合航空宇航科学与技术学科研究生教学基地实验室建设项目“中继系统星间链路天线指向控制系统教学与演示实验” ,以我国跟踪与数据中继卫星系统为背景,对某型号用户星星间链路天线指向跟踪控制和复合控制理论进行深入的研究,研究内容主要包括以下几个方面: 1 .利用lagrange方程建立了用户星的动力学方程,同时推导了运动学方程,并将这组动力学方程以矩阵微分方程形式表示,使之适用于姿态控制系统的设计和分析。