The design and realization technology suitable for integrated real-time simulation device of UAV flight control are presented. The practice and application is emphasized.
本文给出了适于无人机飞行控制的集成化实时仿真设备的设计与实现技术，着眼于工程实践和应用。
The fly-by-light system is demonstrated with a prototype based on fibre channel protocol which has been applied to communications between flight control system and flight simulation system.
该系统通过实现了一个基于光纤通道协议的原型系统得到验证，已成功应用于飞行控制系统与飞行仿真系统之间的通信。
Simulation result indicates that the equivalent moment derivatives model can be used in the evaluation of aircraft conceptual design and flight control system design.
验证表明，等效力矩导数模型可用于评估设计方案或指导飞行控制系统设计。
As part of this, Boeing chief pilot Mike Carriker conducted a simulation that tested each flight control, hardware, and software system.
作为这项工作的一部分，波音公司的首席飞行员迈克·卡里克进行了模拟测试的每一个飞行控制，硬件和软件系统。
Taking the lateral flight control system of an aircraft as an example, simulation was carried out for the cases with perturbing parameter and interference.
以某型飞机侧向飞行控制系统为例，针对系统参数摄动和承受有界干扰情况，对所提出的方法进行了仿真分析与验证。
Finally, the flight control system of an ASV was designed based on the proposed method. Simulation results demonstrate the effectiveness and robustness of the approach.
最后利用所提出的控制方案设计了ASV飞行控制系统，仿真结果表明了控制方案的有效性和鲁棒性。
This new control method is compared with the traditional one by computer simulation, and a dynamical analysis of the control system is conducted for the whole flight process.
进行了新方法与传统控制方法的对比及整个飞行过程的控制系统的动态仿真。
A fire control simulation system for flight simulator based on MIL-D-1553B bus consists of a fire control simulation computer, a fire control simulation console and power supply.
基于1553B总线的载机火控模拟系统，由火控模拟计算机、模拟发控台和电源组成。
Due to mission profile , launched conditions and trajectory , maneuver chains for stand off missile are designed . instruction control model and maneuver model is setup for ucav flight simulation.
结合作战任务剖面、导弹发射条件和弹道，设计出无人机防区外攻击导弹发射前、后的机动动作链。
The general test platform for actuator in flight control system is essential for the design and test of actuator's static and dynamic performance, impedance characteristic and its failure simulation.
飞控作动系统通用测试环境是检验飞机作动系统的动静态性能、阻抗特性、舵机故障模拟和试飞技术支持的重要途径。
The 3-axis flight table is an important device and a typical high performance position and speed servo system used in the hardware-in-the-loop simulation of flight control system.
三轴飞行模拟转台是用于飞行控制系统半实物仿真的高性能位置跟踪和速度跟踪的一个重要设备。
The 3-axis flight table is an important device and a typical high performance position and speed servo system used in the hardware-in-the-loop simulation of flight control system.
三轴飞行模拟转台是用于飞行控制系统半实物仿真的高性能位置跟踪和速度跟踪的一个重要设备。
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