rotor aircraft

The rotor system locates in an aircraft flying with an asymptotic acceleration.

研究渐变加速的飞行器内碰摩转子系统的非线性特性.

A complete tilt rotor aircraft flight control model was developed to enable design of tilt rotor aircraft.

建立倾转旋翼机数学模型是设计其合理的飞行控制律的基础。

Synthesis of Remote Control System of a Small Tilt Rotor Aircraft

遥控小型倾转旋翼机飞行控制系统研究

Modeling of a tilt rotor aircraft platform

倾转旋翼机模拟平台建模与仿真

Full Envelope Flight Control Method for Small Unmanned Tilt Rotor Aircraft

小型无人倾转旋翼机全模式飞行操纵控制

The multi-body analysis of the aeroelastic stability of the tilt rotor aircraft is presented.

通过多体动力学方法建立了倾转旋翼机动力学分析模型.

This mathematical model could be used for design and simulation of the control system of tilt rotor aircraft.

该数学模型可为倾转旋翼航空器的控制系统设计与仿真提供参考。

The design of helicopter and advanced high speed tilt-rotor aircraft is addressed using a series of optimization procedures.

本文研究最优化设计技术在直升机和倾转旋翼机设计过程中的应用。

An adaptive neural networks controller is designed for tilt rotor aircraft platform.

采用自适应神经网络控制方法,设计出倾转旋翼机模拟平台姿态角控制器.

Mathematical model and formulations of a new tilt-rotor aircraft for aeroelastic stability analysis

新型倾转旋翼机气动弹性稳定性分析模型

Research of Dual Model Reference Adaptive Control System for Tilt-Rotor Aircraft

倾转旋翼机模型参考自适应双重控制系统研究

By this method, the characteristics of tilt-rotor aircraft flowfield in hover are investigated. Also, further investigations are conducted to simulate the flowfield of tiltrotor aircraft at different forward-flight speed conditions.

应用该方法，着重研究了悬停状态下倾转旋翼机的流场特性，并对不同前飞速度时的流场也进行了数值分析。

Modeling study on tilt-rotor's aeroelastic stability in cruise flight Surface Improvement Based on Springback Compensation for Aircraft Skin Stretching Tool

前飞状态倾转旋翼机气弹稳定性建模基于回弹的飞机蒙皮拉形模型面修模技术研究

The simulation on the coupled tilt-rotor/ wing/ fuselage flowfield of tilt-rotor aircraft is a challenging and important subject in the field of Helicopter Aerodynamics.

倾转旋翼机旋翼/机翼/机身组合流场的模拟是直升机空气动力学领域具有挑战性和重要意义的研究内容。

Adaptive Neural Networks Control for Tilt Rotor Aircraft Platform

倾转旋翼机模拟平台自适应神经网络控制

An analytical model of tilt-rotor/ pylon/ wing coupled aeroelastic stability is presented and the dynamic equations are derived for a new semi-articulated, soft-inplane tilt-rotor aircraft.

针对新型半铰接式、摆振柔软的倾转旋翼机，建立了旋翼/动力舱/机翼气动弹性稳定性分析模型，并导出了系统的动力学方程。

The platform is quite simple, relatively unexpensive, and very safe, so it provides an excellent experimental platform for research on tilt rotor aircraft.

另外，该平台是一个高阶非线性系统，在一定程度上像倾转旋翼机，为更进一步研究倾转旋翼机提供了很好的实验平台。