飞行器的例句大全

Furthermore, how the Focus-of-Expansion and the Horizon are extracted from a few calibrated sequential images is first introduced, then the aircraft approach angle is derived from these parameters.

首先给出了从已标定的图像序列中提取FOE和Horizon的方法，然后由这两个参数估计出飞行器的接近角。

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。

Now as the craft enters your plane a distortion occurs.

于是,当飞行器进入你们的层面,就会发生一种扭曲.

A new design method for a Flapping Micro Air Vehicle ( FMAV ) was proposed background of engineering application.

提出了适合工程实际的微扑翼飞行器的设计方法.

It provides a theory foundation to design and develop bionic flying micro-robots.

这为设计和研制微型仿生扑冀飞行器提供了理论依据.

Pitch-yaw coupling can be neglected only for nearly axisymmetric vehicles.

只有对接近于轴对称的飞行器,俯仰与偏航的耦合才能略去.

Analysis of Error Sources for Circumlunar Spacecraft Orbit Determination

影响环月飞行器定轨精度的误差源分析

Attitude Control Based on Neural Networks for Micro Aerial Vehicle with Flapping Wings

基于神经网络的拍翅式微型飞行器姿态控制

For attitude control of micro aerial vehicle with flapping wings, a control method based on BP ( backpropagation) neural networks and average moments is proposed.

对于拍翅式微型飞行器姿态的控制，提出了一个基于BP神经网络和平均力矩的控制方案。

Combined with blade element theory, the results can be used to evaluate aerodynamic characteristics of flapping wings, which are helpful for the initial design of micro rotary and flapping wing.

运用本文方法分析了各参数对翼型气动特性的影响，进一步结合叶素理论还可以估算扑翼的气动特性，进而指导微旋翼或扑翼微型飞行器的初期设计。

Measurement and analysis of lift of micro air robot with flapping wings

扑翼式微型飞行器的升力测量与分析

It'should be pointed out that some launch vehicles or missiles are usually unstable.

应该指出,某些发射飞行器或导弹总是不稳定的.

Each orbiter was designed to be reused up to 100 times.

每个飞行器设计为可以重复使用一百次.

The precision estimation of RCS is very important for aerocraft stealth design.

目标RCS的精确计算和预估是飞行器隐身设计极其重要的一部分.

The Vimanas-The Ramayana describes a Vimana a double-deck, circular ( cylindrical ) aircraft with portholes and a dome.

维曼拿斯 —— 《罗摩衍那》描述了维曼拿斯是双重的碟子, 圆形 ( 或柱形 ) 的飞行器,带有舷窗和圆顶.

MIRV ( multiple independently targeted reentry vehicle )

多弹头分导再入飞行器 ( 多弹头导弹 )

Spacecraft reentry trajectory optimization is a kind of optimal control problem.

飞行器再入轨迹优化是一类最优控制问题.

The estimation state for high velocity reentry vehicle is an important subject in the modern defence.

高速再入飞行器的状态估计是现代国防研究中的重要课题.

High-speed reentry aerocraft is usually with terminal guidance system.

高速 再入飞行器通常具有末制导系统.

Affected by unsteady atmosphere disturbance, attitude control and navigation for MAV flight must be unconventional.

针对在非定常大气扰动作用下, 微型飞行器MAV姿态稳定控制与导航都不同于常规的问题.