直升机光电系统网络协同目标瞄准方法北大核心CSCD

针对直升机网络化和信息化的探测需求,提出了利用数据链信息快速引导机载光电系统实现目标瞄准的方法。分析网络信息引导过程中光电系统的目标瞄准指示误差,给出目标信息坐标转换和延迟处理算法以及光电系统瞄准线偏差估计方法,最后通过仿真实验重点研究了数据精度、数据率、延迟时间等对直升机光电系统网络协同目标瞄准的影响。仿真结果表明:减小数据延迟时间,提高数据率和数据精度是减小网络协同目标瞄准误差的有效途径,采用合理的目标信息延迟处理算法,对提高目标状态估计精度,减小目标瞄准线估计误差具有一定的作用。     

基于Mantis的某型直升机视景系统设计与实现

对直升机视景仿真系统的构建进行了分析,针对其对场景细节要求高,需多种特效库支持的特点,首次提出了一种基于Mantis的直升机视景系统的解决方案。该方案利用TerraVista制作精细的地形数据库,经转换后可采用大地形调度技术进行渲染;利用Creator制作三维模型库;采用内容定制文件配置场景中的实体和特效;采用Mantis Client和Mantis Server实现视景的渲染,最后通过基于通用图像生产协议的网络通信控制场景中的目标与特效。实际仿真结果显示,该直升机视景系统的仿真效果形象逼真,满足了实时性需求。     

基于IGRA-ISVD约减和RBF的森林火灾消防直升机需求预测模型

针对森林火灾消防直升机需求预测问题,提出了一种基于改进灰色关联分析(IGRA)和改进奇异值分解(ISVD)约简的径向基函数(RBF)神经网络预测模型.首先,基于既有研究梳理了森林火灾消防直升机需求预测指标体系;然后,在改进灰色关联分析和奇异值分解方法的基础上,分别对消防直升机需求预测数据信息进行属性约简和维度约简;最后,利用约简预测数据信息对RBF神经网络进行训练,进而构建消防直升机数量预测模型.案例分析和对比分析表明了本文所提方法的可行性和合理性.     

Design of helicopter rotor blades with actuators made of a piezomacrofiber composite

For reducing the vibration and noise of helicopter rotor blades, the method of their controlled twisting by using built-in deformation actuators is employed. In this paper, the influence of various design parameters of the blades, including the location of actuators made of a piezomacrofiber material, on the twist angle is evaluated. The results of a parametric analysis performed allowed us to refine the statement of an optimization problem for the rotor blades. __________ Translated from Mekhanika Kompozitnykh Materialov, Vol. 44, No. 1, pp. 77–86, January–February, 2008.     

基于LQR的无人直升机姿态控制器设计

无人直升机控制系统是一个易受环境干扰的、各通道相互耦合的非线性系统.为了实现无人直升机能在不同环境下自主飞行,需要设计抗干扰能力强的控制器;采用系统辨识的方法得到直升机横向通道和纵向通道姿态环路的线性系统模型;根据线性最优二次型理论,对直升机横向通道和纵向通道的姿态环路设计了LQR最优控制器,使用MATLAB仿真选取最优控制器参数后,在ALIGN 700N 直升机上进行了实际飞行试验,仿真和飞行试验表明,采用LQR控制技术设计的无人直升机姿态控制器具有较强的鲁棒性和实用性.     

直升机防撞激光雷达综合信息处理系统

设计了一种新型直升机载防撞激光雷达综合信息处理系统。通过对直升机姿态信息的捕获和修正、目标提取与识别、数据三维空间转换等技术,设计并实现了直升机载激光雷达的改进综合信息处理及显示,并且采用扫描成像激光雷达的探测试验对以上技术进行了实际验证。试验结果表明：该系统有效减小了直升机机动飞行时激光雷达探测画面的畸变,在横滚角30°时仍可有效修正探测图像;另外,在600 m处完成了对电力线等不易观察高危目标的迅速提取;实现了探测画面的三维综合高效显示,综合处理时间〈10 ms。本文提出的新的直升机载激光雷达综合信息处理方式有效改良了人机界面。     

An investigation of open-loop and inverse simulation as nonlinear model validation tools for helicopter flight mechanics

The nonlinear model validation techniques of open-loop and inverse simulation are introduced. The methodologies are explained and examples are given. The paper presents the results of an investigation into the use of open-loop and inverse simulation to help in the development of a nonlinear real-time helicopter model. The individual rigid body state equations in the model are simulated with the aim of producing insight into the cause of inaccuracies in the model. A suspected source of inaccuracy is verified using partial open-loop simulation. Unmodelled dynamics are represented by using the relevant flight data as an open-loop input to the simulation thus revealing the effect of incorporating those dynamics. After localising the cause of inaccuracies in the simulation model, modifications and improvements are verified using closed-loop simulation. The improvements are then evaluated by comparing results in normal and inverse simulation modes.     

Demonstration of a coupled floating offshore wind turbine analysis with high-fidelity methods

This paper presents results of numerical computations for floating off-shore wind turbines using, as an example, a machine of 10-MW rated power. The aerodynamic loads on the rotor are computed using the Helicopter Multi-Block flow solver developed at the University of Liverpool. The method solves the Navier–Stokes equations in integral form using the arbitrary Lagrangian–Eulerian formulation for time-dependent domains with moving boundaries. Hydrodynamic loads on the support platform are computed using the Smoothed Particle Hydrodynamics method, which is mesh-free and represents the water and floating structures by a set of discrete elements, referred to as particles. The motion of the floating offshore wind turbine is computed using a Multi-Body Dynamic Model of rigid bodies and frictionless joints. Mooring cables are modelled as a set of springs and dampers. All solvers were validated separately before coupling, and the results are presented in this paper. The importance of coupling is assessed and the loosely coupled algorithm used is described in detail alongside the obtained results.     

High-resolution multi-code implementation of unsteady Navier–Stokes flow solver based on paralleled overset adaptive mesh refinement and high-order low-dissipation hybrid schemes

The low-dissipation high-order accurate hybrid up-winding/central scheme based on fifth-order weighted essentially non-oscillatory (WENO) and sixth-order central schemes, along with the Spalart--Allmaras (SA)-based delayed detached eddy simulation (DDES) turbulence model, and the flow feature-based adaptive mesh refinement (AMR), are implemented into a dual-mesh overset grid infrastructure with parallel computing capabilities, for the purpose of simulating vortex-dominated unsteady detached wake flows with high spatial resolutions. The overset grid assembly (OGA) process based on collection detection theory and implicit hole-cutting algorithm achieves an automatic coupling for the near-body and off-body solvers, and the error-and-try method is used for obtaining a globally balanced load distribution among the composed multiple codes. The results of flows over high Reynolds cylinder and two-bladed helicopter rotor show that the combination of high-order hybrid scheme, advanced turbulence model, and overset adaptive mesh refinement can effectively enhance the spatial resolution for the simulation of turbulent wake eddies.