半物理仿真

该半物理仿真平台经合作单位试验测试，平台各项技术指标满足项目计划要求，并通过厦门市科技局组织的专家组验收。

The HILS platform have been tested by the cooperative company , all of the technique index satisfy the program requests , and the HILS platform has passed the checking which was carried out by the Science and Technology Bureau of Xiamen .

半物理仿真系统中OPC数据监控子系统

Data Control Subsystem Based on OPC in Semi-physical Simulation

针对半物理仿真要求，基于VC++编译环境用C语言实现了捷联惯性/天文组合导航算法，并进行了实验验证。

For the demand of semi-physical simulation , realize algorithm of the integrated navigation with C language which based on VC + + compile environment and verified by experiment .

通过半物理仿真试验结果证明，所设计的模糊PID控制系统实现了快动态和高精度的统一。

After hard ware in the loop simulation test , its result proved that the designed fuzzy PID control system can achieve fast and high-precision .

在此模型的基础上，利用DELTA手控器，对柔性物体接触变形以及实时虚拟力反馈进行半物理仿真。

Based on the model , DHD ( Delta Haptic Device ) is able to reveal the contact force through touching the virtual soft object .

针对导弹半物理仿真系统高精度定时问题，设计了在Windows操作系统下基于软件定时的解决方案。

For the issue of high accuracy timing of hardware-in-the-loop simulation for missiles , the software timing solution based on Windows OS has been presented in this paper .

基于xPC的小卫星半物理仿真验证平台

Hardware-in-Loop Simulation Platform for Small Satellite Based on xPC Real-time Simulator

基于Bladed的电液比例变桨距风力机半物理仿真平台

Semi-physical Simulation Test-bed for Electro-hydraulic Proportional Pitch-controlled Wind Turbine System Based on Bladed

RTW在某型直升机飞控系统半物理仿真中的应用直升飞机飞行动力学

Application of RTW in a Helicopter Flight Control System Hardware-in-the-loop Simulation

基于xPC的挠性天线跟踪指向系统半物理仿真

XPC-based hardware-in-the-loop simulation for flexible antenna tracking and pointing system

小卫星姿控xPC半物理仿真系统设计

Design of xPC semi-physical simulation system for small-satellite attitude control

在dSPACE实时仿真平台上进行半物理仿真实验，调定各个关节电机的控制参数。

The motor control parameters are set up for each joint in dSPACE real-time simulation platform .

利用现代V模式开发流程，研究柴油机电控系统从功能设计、快速原型、代码生成到半物理仿真的一体化仿真技术，解决电控系统开发、调试难题是十分必要的。

The integrated simulation technology was used to research the diesel electronic control system which is from the functional design , the rapid control prototyping , the code generation to semi-physical simulation .

其次，对GPS导航系统进行描述并半物理仿真实验。

Based on the simulation results , a appropriate state equation model is provided for relative navigation . Secondly , the GPS navigation system is described and a semi-physical simulation experiment of GPS is carried .

基于DCPS的分布式多UCAV协同控制半物理仿真系统

Distribute Semi-Physical Simulation System for Multi UCAVs Cooperative Control Base on DCPS

通过PLC结合变频器、电机以及旋转平台的形式构建一个船舶运动的半物理仿真系统来模拟实际船舶的运动姿态。

We simulate the motional status of the actual ship by means of designing a ship manoeuvrability semi-physical simulation system , which can be formed by PLC combined with the frequency converter , motor and rotating platform .

用C语言编制控制软件，为了验证控制软件的正确性，建立了半物理仿真系统，对刹车控制系统、位置控制系统、载荷控制系统、能量控制系统进行了连接和检验。

Control software is written in C language . The semi-physical simulation system is setup to test the software . After that , the brake control system , the position control system , the load control system and the energy control system are combined together and inspected .

基于理论研究，通过dSPACE实时仿真平台进行了实验样机的半物理仿真实验研究，证实了理论分析的正确性和方法的实用性。

Based on both theoretical analysis and semi-physical simulation based on the platform of dSPACE real-time simulation system , the theory is proven and approaches are effective .

最后，采用发动机试车的方法对发动机控制系统的性能和功能进行检验，并使用半物理仿真的方法验证自适应PID控制器的控制效果，所得结果满足无人飞行器飞行控制要求。

Finally , engine tests were built to validate the capability and functionality of ECS and a hardware-in-the-loop simulation experiment was conducted to verify the control performance of adaptive PID controller . The results show the ECS meet the requirement of UAV flight control .

通过使用简化模型方法，分析了一种半物理仿真（HILS）试验用运动模拟试验转台的基本动态要求。

By using a simplified model , the dynamic requirement of motion simulator used in hardware-in-the-loop simulation are derived in this paper .

基于dSPACE半物理仿真系统对绳索牵引机器人进行了实验研究，主要包括机器人的驱动控制特性实验和轨迹跟踪实验等。

Based on the dSPACE system , the experimental study was conducted , which mainly included . the actuation control characteristic experiment , the trajectory planning experiment and so on .

从已建立的模型出发，对全数字仿真系统软件和半物理仿真系统的软硬件进行设计，并分别在LabWindows／CVI平台下进行仿真软件的程序实现。

Using these models , the software of full digital system and both the software and hardware of semi-physical simulation system are designed . Then the programme of two softwares is realized under LabWindows / CVI environment .

建立了半物理仿真系统软件平台和PXI测控系统。

The dynamic simulation model of marine 3-shaft gas turbine engine was established . ( 2 ) The software platform of Hardware-in-the-Loop simulation system and PXI measurement & control system was developed .

基于dSPACE半物理仿真系统和所研制的压电作动器，设计并构建了智能天线结构实验平台，进行了结构变形控制实验研究。

With dSPACE simulation system and developed piezoelectric ceramic actuators , an intelligent antenna structure was designed and founded as a testbed and the experiments concerned of deformation control were developed in this work .

为了验证导航算法的性能，以导航算法能最终实现工程应用为背景，文中研究了一种以RS-232串行通信为基础，采用分布式仿真结构的多信息融合组合导航半物理仿真系统。

In order to confirm the performance of the navigation algorithm , and finally apply this algorithm into engineering project , one distributed multi-information fusion integrated navigation semi-physical system is studied , which is based on RS-232 serial communication .

并基于dSPACE半物理仿真系统对绳驱动助行机构系统进行了实验研究，主要包括控制系统的驱动控制特性试验，不同条件下的轨迹跟踪试验和减重步态康复训练控制实验。

And then the experimental study was conducted based on the dSPACE system , which mainly included the actuation control characteristic experiment , the trajectory planning experiments with different experimental conditions and the gait rehabilitation training weight control experiments .

在直升机显模型跟踪电传飞行控制系统（MFCS）的基础上，开发了直升机贴地飞行波分复用光传系统实时半物理仿真验证平台。

Based on the explicit model-following Fly-By-Wire ( FBW ) control system of the helicopter ( MFCS ), a real-time semi-physical nap-of-the-earth platform is established and a simulated fly test is processed .

论文从介绍半物理仿真技术和发动机数控系统入手，在分析了发动机数控系统半物理仿真试验整体结构的基础上，提出了一种基于RS232串口通信的接口信号仿真器设计方案。

Starting with the presentation of semi-physical simulation technique and engine digital control system , the paper brings out , on the basis of analysis of main design for semi-physical simulation of engine digital control system , a designed scheme of signal interface emluator that derives from RS232 serial port .

重点针对星敏感器和速率陀螺联合定姿算法、喷气bang-off-bang时间最优控制律算法、反作用飞轮四元数反馈稳态控制律算法分别设计了半物理仿真实验。

Designed semi-physical simulations emphasized on attitude determination algorithm based on star sensor combined with gyroscope , bang-off-bang time-optimal jet control algorithm , and quaternion feedback control algorithm using flywheel .

同时，半物理仿真对加速工程机械产品的开发周期具有重要意义。

HIL simulation can shorten the development cycle of construction machinery .