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That drone was meant for her, not us. It was revenge.

上次那个飞行器是去杀她的,不是我们,是一次复仇行动。

Indeed the structures of flight vehicles are very flexible when compared with bridges, buildings, and earthbound machines.

实际上,与桥梁、建筑和地面上的机器相比,飞行器结构是非常灵活的。

It is an important half hardware-in-loop simulation equipment, which is often used to simulate the aerodynamic torque load on the missile rudder or elevon actuators in the flight.

它是地面半实物仿真系统中的一种重要专用设备,用来模拟飞行器舵机在飞行过程中所承受空气动力力矩载荷。

Aiming at the composition of shipborne UAV system and the main problems in its embarkment on ships,this paper analyzed and proposed the model selection requirements on the three subsystems(aerocraft,task equipment and ship surface system) of the shipborne UAV system,and brought forward suggestions on development thoughts of shipborne UAV system.

针对舰载无人机系统的组成以及上舰存在的主要问题等进行分析,提出舰载无人机系统三个子系统(飞行器、任务设备、舰面系统)的选型要求,对舰载无人机系统的发展思路提出建议。

Information such as attitude angle of aircraft is used to emendate the large-geometry-distorted image, so the research of this dissertation is based on the hypothesis that images used have small geometry distortion.

针对图像匹配在导航中的应用,提出了对于存在大的几何失真的图像利用飞行器本身信息进行几何校正的方法,所以本文算法的研究都是基于小的几何失真这一假设的。

Information such as attitude angle of aircraft is used to emendate the large-geometry-distorted image, so the research of this paper is based on the hypothesis that images used have small geometry distortion and invariant moment feature is used to reduce this distortion.

由于大的几何失真图像可利用飞行器本身信息进行几何校正,所以本文的研究都是基于小的几何失真这一假设的,并且利用不变矩特征来减小这种失真。

The drone flies autonomously enroute to its patrol area its radar seeker head constantly search for hostile radars.

无人飞行器飞行中自主到它的巡逻区域,它的雷达搜索头不停地寻找敌方雷达。

An algorithm for estimating aircraft approach angle using computer vision is proposed in this paper.

提出了一种基于图像序列的飞行器接近角的估计方法。

Using Eulerian angle information in rudder-control-loop is a general method in the strapdown inertial navigation system of aerocraft.

在舵偏控制回路中使用欧拉角姿态信息,是现有飞行器捷联惯导系统普遍采用的方法。

The structure of flow field and the aerodynamics along with the inner energy excitation and the variable flow conditions were analyzed in details.

采用L-B碰撞模型,分析了内能激发松弛的流场参数特性,从分子碰撞、分子与飞行器表面碰撞的角度,分析了不同来流条件下的流场参数的变化情况。

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