机动飞行

海豚型直升机转弯机动飞行特性研究

Study on Z-9 Helicopter Turning Maneuver Characteristics by Energy Method

飞机机动飞行时的隐模型控制器设计

Controller Design by the Implicit Model-Following Technique in Maneuver

3DSTUDIO在飞机机动飞行科目中的应用研究

Applied research on 3D Studio Software in aircraft maneuver flight test

INS具有抗电子干扰、大机动飞行、隐蔽性好的特点。

INS has anti-jamming , high dynamic flight and concealment features .

简述了采用3DSTUDIO软件后，给飞机机动飞行科目试飞结果分析带来的重要变化。

This paper presents the important change brought about by the 3D STUDIO software in aircraft maneuver flight-test result analysis .

BTT导弹机动飞行非线性解耦控制

Nonlinear decoupling control for bank-to-turn missile

机动飞行条件下带挤压油膜阻尼器的Jeffcott转子系统的振动特性

The Vibration Performance of the Jeffcott Rotor System with SFD in Maneuver Flight

仿真结果表明奇偶向量补偿算法可大大提高FDI的性能，特别是在飞行器做机动飞行时。

In this paper the problem of noise compensation for FDI systems is also presented . Simulation result shows that the parity vector compensation algorithm can significantly improve FDI performance , especially during vehicle maneuvers .

本文建立了位于机动飞行飞行器内且同时具有初始弯曲、不对称刚度和质量不平衡的单盘Jeffcott转子的动力学模型。

A mathematical model of an unbalanced rotor system located in aircraft with asymmetric rigidity and initial bending is given in this paper .

机动飞行，如快速拉杆、荷兰滚等也会产生较大的1P载荷。

The maneuvers flight , such as pull quickly back on the stick , bumping , induce greater 1 P loads .

主要的内容包括直升机飞行控制系统内外回路设计、直升机机动飞行的仿真、地形跟随的仿真以及OpenGL三维动画仿真等方面的内容。

In this paper involved several aspects about the inner and outer loops design for helicopter flight control system , maneuver flight simulation for helicopter , terrain following simulation and 3D animation flight simulation system designed with OpenGL .

对于机动飞行过程，建立了水平盘旋、俯冲拉起两种机动飞行附加载荷的计算模型和机动飞行下Jeffcott转子的运动微分方程，并对转子的振动特性进行了仿真。

The maneuver load model for hover and dive-hike are set up , and the motion equations for Jeffcott rotor in maneuver flight are derived .

本文讨论了高机动性飞机滚转机动飞行对纵横航向操纵效能的要求，并以J-7飞机为算例进行了验证。

The longitudinal and lateral directional control effectiveness requirements of high maneuver aircraft are discussed in this paper , and the fighter J-7 is taken as an example .

为验证综合模型的有效性，以UH-60A直升机为例，进行了定常平飞配平计算以及右压杆、急拉杆机动飞行的动态响应计算。

To validate the comprehensive model , the UH-60A helicopter is taken as an example to predict the trim characteristics and dynamic responses in maneuvering flight .

以SH-2G为控制对象，采用基于神经网络的非线性系统反馈线性化控制方法，进行直升机机动飞行仿真。

A maneuver simulation of the helicopter , modeling of SH-2G , is performed by using the nonlinear system control technology for feedback linearization based on neural network .

国外某型机载火控系统中，采用了一种改进的CCRP轰炸瞄准原理，在机动飞行过程中，同时完成方向瞄准与距离瞄准，从而简化了瞄准过程。

An improved CCRP bombing principle was adopted in a certain kind of foreign airborne fire control system , which can complete the direction aiming and distance aiming at the same time during maneuvering flight .

本文介绍了机动飞行中俯仰动态反应的三个判别准则，并通过J-7飞机的试飞，测量和计算了这些判据，以便比较和验证这三个准则的适用性。

In this paper , three specifications of pitch dynamic response in maneuvering flying are presented . In flying test of a J-7 aircraft , these judged criterions were measured and computed , so that these specifications are compared and proofed according to their suitability .

从水平机动飞行中确定航程性能的试飞方法

Flight test method determing the range performance from level maneuver flight

机动飞行飞行器内具有初始弯曲和刚度不对称的转子运动模型

Mathematical Modeling of a Maneuvering Asymmetric Rigidity Rotor with Initial Bending

适用于机动飞行目标跟踪的半自动光学引导系统

The Semiautomatic Optical Guiding System Used in the Mobile Aero-target Tracking

机动飞行时发动机转子系统动力学统一模型

General dynamic model of aeroengine 's rotor system during maneuvering flight

战斗机超机动飞行自抗扰控制器设计

Auto-Disturbances Rejection Controller Design of Aircraft Super - Maneuverable Flight

当导弹作高机动飞行时，线性理论将不再成立。

The linear theory is no longer available when missile flies flexibly .

飞机大迎角机动飞行控制律研究

Control law study of aircraft maneuvers at high attack angle

小型无人机尾翼对称机动飞行载荷计算

Flight Maneuver Loads Calculation of the Small UAV 's Tail

导弹纵向机动飞行的非线性鲁棒控制研究

A Study of Nonlinear Robust Control of Longitudinal Maneuvering Flight for Missiles

大机动飞行情况下姿态控制系统的设计

The Design of attitude control system for large maneuvering aircrafts

飞机大机动飞行的一种模糊控制系统设计方法

Design Method of Fuzzy System to Control Large Maneuver Flight of Aircraft

飞行器机动飞行时发动机转子等变速运动的动力学特性研究

Dynamics of a maneuvering rotor in constant acceleration and deceleration

太空飞行器机动飞行飞机场上有十架飞机。

Spacecraft maneuver There is ten planes in the airfield .