侧滑角

模糊神经网络的侧滑角校正

Calibration of angle of sideslip using fuzzy neural network

叙述了一种利用模糊神经网络模型来校正侧滑角的方法。

This paper describes a method of angle of sideslip calibration using a fuzzy neural network model .

其次，选取了ModelA作为基准进气道，就不同侧板位置（即侧板遮挡度）进气道在不同马赫数以及不同侧滑角飞行条件下的性能展开了研究。

Secondly , with Model A as a base , the performance of inlets with sidewalls on different locations ( degree of sidewall shade ) under different Mach number and sideslip angle were studied .

一种基于INS的攻角和侧滑角测量算法

An Estimation Method of Angle-of-attack and Sideslip Angle Based on INS

目前国际上X射线干涉仪所采用的微动工作台均采用对称式柔性铰链结构，其缺点是侧滑角大，严重影响干涉信号的对比度，很容易产生干涉条纹的记数误差。

Traditional X ray interferometer normally use symmetrical translation stage It causes large yaw angle of analyzer , this seriously influences the contrast of x ray interference signal .

本文介绍了两种方法来得到迎角和侧滑角的虚拟传感器信号：非线性观测器方法和利用INS／GPS系统数据估计迎角和侧滑角方法。

This paper introduces two methods to get the virtual sensor signal of angle of attack and sideslip angle : Nonlinear Observer method and INS / GPS method .

对横侧向而言，为了消除侧滑角对飞行控制带来的影响，提高转弯效率，采用倾斜转弯（BTT）控制方法设计了横侧向姿态飞行控制系统。

In lateral subsystem , we use BTT control method to design attitude control system in order to eliminate the effect of slip angle and improve cornering efficiency .

以炮弹飞行时的攻角、侧滑角与滚转角为状态变量，结合弹道飞行参数与MEMS陀螺/GPS测量数据，建立了非线性姿态滤波估计状态方程与量测方程。

With the angle of attack , the sideslip angle and roll angle as the state variables , the nonlinear attitude filter estimated state equations and measurement equations were established combined with ballistic parameters and the MEMS gyroscope and GPS measurement data .

本文研究的对象是以小迎角、小侧滑角和一般超音速飞行的旋转弹翼式X-X型导弹。

A missile with tilt-wings in " X-X " configuration is considered in supersonic flight at small angle of attack and sideslip angle .

为了提高飞航导弹的侧向机动能力且保证导弹不产生较大的侧滑角（受导弹所用发动机进气道限制），本文探讨倾斜转弯（BTT）控制在飞航导弹控制中的有关理论与应用问题。

This paper discusses the problem of guidance and control for bank to turn ( BTT ) winged missile for improving its lateral maneuverability while maintaining a small sideslip angle ( limited by the engine in let ) .

研究了采用纵横向耦合且具有线加速度反馈的非线性观测器方法，该方法能够同时估计迎角和侧滑角参数，并采用Extrem优化方法对其反馈参数增益参数进行了优化设计。

The observer using the coupling of axial and lateral and having feedback of acceleration is investigated . This method can estimate the angle of attack and the sideslip angle synchronously . An optimization named Extrem is applied to optimize the feedback plus matrix .

直升机旋翼/机身组合模型的带侧滑角风洞试验

Rotor / Fuselage Compound Model Wind Tunnel Test with Sideslip Angle

飞船返回舱再入飞行迎角和侧滑角估计

Angle-of-attack and sideslip-angle estimation of reentry capsules of spacecraft in reentry flight

飞机攻角侧滑角传感器检测系统

Detection system of aero attack and sideslip angle sensor

它适用于超音速和低的高超音速范围，并可用于中等攻角和侧滑角。

It is valid in the range of supersonic and low hypersonic speeds .

根据飞艇侧滑角姿态跟踪误差值的大小，判断其侧滑角姿态调整范围。

Yaw attitude modulation is judged by tracking error .

本文发展了基于弹道重建的返回舱迎角和侧滑角估计方法。

An angle-of-attack and sideslip-angle estimation method is developed based on trajectory reconstruction .

飞机迎角、侧滑角传感器图像检测系统的研制

Development of image detecting system for the plane 's heading and yawing angle sensors

截短流线跟踪进气道对带攻角或侧滑角飞行比较敏感。

Truncated streamtraced inlet is sensitive to the flight at angles of attack or sideslip .

侧滑角速度导数对飞机动态特性影响

A study of the effects of the lateral acceleration derivatives on dynamic characteristics of aircraft

大多数飞行状态都要求保持侧滑角等于零。

In most flight conditions it is desired to maintain the sideslip angle equal to zero .

低速来流大攻角侧滑角状态下尖脊进气道气动特性试验研究

Experimental Investigation on Gas-Dynamic Performance of Caret Inlet under Condition of Large Attack Angles and Yaw Angles

有侧滑角椭圆弹身大攻角状态绕流的数值模拟

State Painting The Numerical Simulation of Flow Around an ElliPtical Body at Roll Angle and High Incidence

小米曲奇饼干，是从本地资源出发，遵循品质及营养平衡的原则，选用营养价值较高的晋谷16号，质优的小麦面粉为主要原料制作而成。模糊神经网络的侧滑角校正

Rom the angle of local resources and the balance Calibration of angle of sideslip using fuzzy neural network

有侧滑角的非对称体超音速无粘绕流的数值计算和近似计算

Numerical and approximate methods for computing steady INVISCID SUPERSONIC FLOW OVER non-symmetrical body with angle of side slip

弹射救生系统大迎角大侧滑角天平设计研究

A Big Cheater Development of the balance for crew escape system at large angles of attack and sideslip angles

亚、超音速小侧滑角机翼升力面理论和数值计算方法

Lifting surface theory and the numerical method of wings with small angles of sideslip at subsonic and supersonic speeds

人们可以看到，侧滑角和方向舵偏角都在很大程度上依赖于爬升角。

Both the sideslip angle and the rudder angle are seen to be very much dependent on the angle of climb .

迎角和侧滑角是飞船返回舱再入飞行试验气动分析工作所需的重要参数。

Angle-of-attack and sideslip-angle are two important parameters for the aerodynamic analysis of reentry capsules of spacecraft from flight test data .

用数值模拟方法研究了椭圆细长体在大侧滑角、大攻角状态下的流动特性。

The characteristics of flow over an elliptical body at 45 ° roll angle and high incidence are investigated by numerical method .