飞行器

Since had own starship, the kind of person robot then starts in the summit sky execution patrol mission, moreover the arrogance is more rampant, has created the very great difficulty to the humanity police power's further bombing, was good jumbles together in the hybrid area senior official with 黒 area senior official black Germany graceful this time has brought the massive long-distance weapon delivery, therefore then stay up till dawn carried on the rug type saturation bombing to the Moon crater base, caused in the crater the kind of person robot not to dare to appear easily, also their flight vehicle after shot down the dozens of frames does not have to remove into in the base to hide.

自从有了自己的星际飞行器，类人机器人便开始在山顶上空执行巡逻任务，而且气焰更加嚣张起来，对人类警察部队的进一步轰炸造成了很大难度，好在混血区长官混为一谈和黒区长官黑德曼这次又带来了大量远程发射武器，于是便日夜不停地对月球环形山基地进行地毯式饱和轰炸，使环形山内类人机器人不敢轻易露头，它们的飞行器在被击落数十架之后也不得撤入基地内隐蔽起来。

Flight motion simulator is one of the most important devices for real-time hardware-in-loop simulation of flight control systems.

随着航空，航天工业技术的高速发展，对半实物仿真技术的要求不断提高，这对仿真设备的执行器和控制器的设计提出了挑战，高性能的控制系统可以为飞行器的性能提供更可靠的试验数据，从而提高飞行器的开发质量和速度。

A vertical component that is too large or a horizontal component that is too small may lead to system instability.

此外，飞行器达到预期加速度的时间长短即飞行器加速度变化的快慢也会大大影响系统的响应。

Research advances and development of hypersonic vehicles in recent years were reviewed, and relevant technologies of hyersonic vehicles were summarized in this paper firstly.

首先回顾了近年来国外高超声速飞行器的研究现状和进展，对高超声速飞行器的一些相关技术进行了总结。

To calculate the aerodynamic forces on the vehicle and grid-fins, we use time-dependent method to solve the Navier-Stokes equation of ideal gas, and flux conservational multizones method to divide the complex vehicle and grid-fins into eight computational zones which are relatively independent, and correlative with each other at once with satisfactory results.

为了计算作用在飞行器和栅格翼上的气动力，采用时间相关法数值求解完全气体的三维Navier－Stokes方程，并运用通量守恒的分区计算方法，将复杂的飞行器和栅格翼系统分解成八个既相对独立，又相互关联的计算区域，得到了满意的结果。

The report has presented detailed research on concerned instances of integrated navigation and compared it with the system of the subsonic vehicle. The research has shown that the scheme composed of Changhe Ⅱ loran, Beidou satellite navigation system and GNSS for such subsonic vehicles is feasible and technically realizable.

本文对有关组合导航的实例进行了详细研究，与亚音速飞行器组合导航系统进行了比较研究，表明亚音速飞行器采用"长河二号"无线电导航系统、"北斗"卫星导航系统和全球卫星导航系统进行组合导航是切实可行的，在技术上是完全可以实现的。

Established the aircraft mathematical model of space motion, application, Newton interpolation polynomial method on the aerodynamic parameters identification, use of C language compiled simulation program, and to out the simulation results and analysis.

详细说明：对某飞行器的全空域飞行弹道进行了仿真研究。建立了飞行器空间运动的数学模型，应用"牛顿插值多项式法"对气动力参数进行了辨识，用C语言编制了仿真程序，并给出了仿真结果及分析。

He probability of low altitude penetration can be highly improved by the TF/TA optimal trajectory planning.

F/TA最优轨迹规划技术可以在很大程度上提高突防飞行器的突防概率，是实现飞行器低空突防飞行的关键技术。

On this basis, anoptimization algorithm library named OPTLIB is formed. The study of dynamic optimization theory is followed. To solve the problem of thecoupling of the static and the dynamic parameters of the flying vehicle design, some auxiliaryvariables are introduced to deal with them together. Then the calculus of variation is adoptedand augment form of Pontryagin's Maximum Principle is derived.

研究了飞行器设计中的典型动态优化问题——轨迹优化问题及算法，针对飞行器设计中的静态参数和动态参数互相耦合的问题，引入辅助变量将静态参数和动态参数统一处理，在此基础上用变分法推导了极大值原理的增广形式，证明了单独的静态或动态最优并不等于总体最优。

In allusion to the condition on the aircraft visual locating ,a method based on Kalman filter to study aircraft position and movement parameter of image sequences is proposed.

针对飞行器的视觉定位问题，提出了基于卡尔曼滤波技术的序列图像飞行器位置和运动参数进行研究的方法。

This one mode pays close attention to network credence foundation of the businessman very much.

这一模式非常关注商人的网络信用基础。

Cell morphology of bacterial ghost of Pasteurella multocida was observed by scanning electron microscopy and inactivation ratio was estimated by CFU analysi.

扫描电镜观察多杀性巴氏杆菌细菌幽灵和菌落形成单位评价遗传灭活率。