1·The attitude control thruster (ACT) is the control component of the flight vehicle.
姿态控制推力器(act)是飞行器控制系统的执行部件。
2·This paper content is the flight vehicle stabilization loop analysis and the design.
本论文的内容是飞行器稳定回路的分析与设计。
3·Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics;
北京航空航天大学 飞行器设计与应用力学系；
4·In this paper, principle, design and test result of MMW wide beam antenna on flight vehicle is introduced.
本文介绍一种用于飞行器上的毫米波宽波束天线的原理、设计方法和实验结果。
5·Error analysis, modeling and compensation of MEMS gyroscope and its application in navigation of flight vehicle are researched in this paper.
本文主要研究了微机电陀螺的误差分析、建模和补偿，以及在飞行器导航中的应用。
6·Assuming that noise is unknown but bounded, set membership identification problem for flight vehicle aerodynamic parameters is studied in this paper.
在噪声未知但有界的情况下，本文研究了飞行器气动参数的集员辨识问题。
7·The results show that optimum design of solid propulsion in single discipline doesn't stand for multi-disciplinary optimum design for flight vehicle system.
结果表明，固体推进单学科的最优设计不等价于飞行器总体多学科的最优设计；
8·When aerodynamic numerical simulation for flight vehicle and its components is conducted, the aerodynamic shape is generally given in the manner of discrete data.
对飞行器及其部件进行气动力数值模拟时，气动外形常常是以离散数据形式给出。
9·With the improving of modern advanced flight vehicle, more and more attentions have been paid to the asymmetric flow involved over slender bodies at high incidence.
随着先进飞行器的性能提高，大攻角非对称流动问题越来越受到重视。
10·In flight vehicle preliminary design it is necessary to quickly and economically estimate the aerodynamics of a wide variety of flight vehicle configuration designs.
在飞行器的初步设计中，快速而有经济地估计出飞行器结构设计中的各种气动特性是非常必要的。