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[Software Engineering03041507

Description: 在某初教机的线性模型基础上,建立了飞机的纵向和横向传递函数,分析了模型参数的不确定性,通过使用MATLAB中的NCD模块对飞行控制系统及PID控制器等参数进行优化,设计出了飞机的自动驾驶仪高度保持和航向保持模式。这种方法既避免了复杂的计算和编程,又使系统具有较好的稳定,陛、动态性能和鲁棒性,克服了飞机模型参数随着高度和速度的变化(即模型参数存在不确定性)而需要按照多个不同高度和速度的飞行区域设计一系列控制器的缺点-early in a plane of the linear model, based on the aircraft's vertical and horizontal transfer function, Analysis of the model parameters of uncertainty, MATLAB through the use of the NCD Blocks flight control system and PID controller parameters for optimization, design of the aircraft's automatic pilot systems, and maintain a high degree course-keeping mode. This method not only avoids the complex calculation and programming, the system has good stability, Her Majesty, dynamic performance and robustness. overcome the aircraft model parameters with the height and speed of change (that model parameters uncertainty exists) and the need to not more than with the height and speed of regional flight controller design a series of shortcomings
Platform: | Size: 277504 | Author: jake | Hits:

[OpenGL programTERRAIN9

Description: 用opengl开发飞机飞行动态的画面,鼠标左键按下可以控制飞行姿态。-Opengl aircraft used to develop dynamic screen, press the left mouse button can control the flight attitude.
Platform: | Size: 138240 | Author: 晁艳普 | Hits:

[Mathimatics-Numerical algorithmssldemo_f14

Description: This demonstration models a flight control for the longitudinal motion of a Grumman Aerospace F-14 Tomcat. First order linear approximations of the aircraft and actuator behavior are connected to an analog flight control design that uses the pilot s stick pitch command as the set point for the aircraft s pitch attitude and uses aircraft pitch angle and pitch rate to determine commands. A simplified Dryden wind gust model is incorporated to perturb the system.
Platform: | Size: 11264 | Author: wanghuixia | Hits:

[transportation applicationsnhlsd

Description: 飞行控制系统中飞机舵回路速度受阶跃干扰时速度保持回路-Flight control system aircraft rudder speed loop interference by step to maintain the speed loop
Platform: | Size: 7168 | Author: duhaitao | Hits:

[OtherClient

Description: 飞机各个飞行阶段的控制规律,速度,速度变化率,高度,等等。-Various phases of aircraft flight control law, speed, speed change rate, height, and so on.
Platform: | Size: 1024 | Author: 朱旭 | Hits:

[OpenGL programMyExplosion

Description: 基于vc++使用opengl编写的飞机飞行模型,实现了飞机的键盘飞行控制和爆炸特效-Based on vc++ using the opengl prepared aircraft model, the realization of the aircraft flight control keyboard and explosive special effects
Platform: | Size: 2093056 | Author: xuchi | Hits:

[OtherAutomaticFlightControlSystems

Description: This an introductory textbook on automatic flight control systems (AFCSs) for undergraduate aeronautical engineers. It is hoped that the material and the manner of its presentation will increase the student s understanding of the basic problems of controlling an aircraft s flight, and enhance his ability to assess the solutions to the problems which are generally proposed.-This is an introductory textbook on automatic flight control systems (AFCSs) for undergraduate aeronautical engineers. It is hoped that the material and the manner of its presentation will increase the student s understanding of the basic problems of controlling an aircraft s flight, and enhance his ability to assess the solutions to the problems which are generally proposed.
Platform: | Size: 16338944 | Author: simon | Hits:

[Software EngineeringARM

Description: 作为无人飞机飞控系统的核心,飞控计算机通常采用基于嵌入式系统的实现方案;ARM嵌入式 处理器及Linux嵌入式操作系统以其一系列优点在飞控计算机中具有广泛的应用前景。本文研究了基于ARM-Linux的某型无人飞机飞控计算机的实现方法, 给出了系统总体设计方案,着重介绍了硬件电路的设计过程,列出了软件调试流程图,分析了调试结果。实践证明,该实现方法结构简单,功能强大,能够满足系统 控制的要求,具有较好的实用性。-As unmanned aircraft flight control system, the core of the flight control computer, usually embedded system-based implementation of the program ARM embedded processors and Linux embedded operating system with its series of advantages in the flight control computer has a broad application prospects. In this paper, based on ARM-Linux for a certain type of unmanned aircraft, flight control computer, the realization of the method to the system design plan, focuses on the hardware circuit design process flow chart listing the software debugging, analyzing the results of the debugging. Practice has proved that the implementation method is simple, powerful, able to meet the requirements of system control, with good usability.
Platform: | Size: 245760 | Author: coffee | Hits:

[ConsoleV0.63

Description: 四轴飞行器飞控主板程序代码V0.63 avr程序代码,飞控板V1.2-Four-axis aircraft flight control board code V0.63 avr code, flight control board V1.2
Platform: | Size: 134144 | Author: | Hits:

[SCMV0.64

Description: 四轴飞行器飞控主板程序代码V0.64 avr程序代码,飞控板V1.2-Four-axis aircraft flight control board code V0.64 avr code, flight control board V1.2
Platform: | Size: 135168 | Author: | Hits:

[SCMsign

Description: 多操纵面战斗机飞行控制系统设计Multiple control aircraft flight control system design-Multiple control aircraft flight control system design
Platform: | Size: 378880 | Author: uu | Hits:

[matlabReconfigurable-flight-control

Description: 精密控制结构需要满足先进飞机的使命和对其引航的要求。这就要求飞行器的性能必须满足在低空飞行,低速飞行和大迎角攻击性飞行,全天候,昼夜工作的条件,并且新的控制技术应该成熟。这项工作提出了飞行控制时,状态变量和控制输入是由预先确定的限制范围内的系统控制系统的设计理念。在设计过程使用动态规划的概念。其基本思想涉及非二次泛函最小化。由于一系列限制因素,建议使用光滑函数。同时提出了该综合方法的优点。我们利用对F-18战斗机的纵向控制配置来说明该设计方法。-Indirect adaptive control for reconfigurable flight control is advocated. Specifically, online static system identification using a moving window/batch estimation is implemented. The ensuing linear regression is augmented with an intercept. The intercept parameter is included to address the effects of trim change associated with the occurrence of a control surface failure. Parameter estimate information is used to adjust the inner loop’s control gains, and a command derived from the intercept estimate is fed forward to automatically retrim the aircraft. The tracking performance of this automatic retrimming method, which relies on system identification, surpasses the conventional approach of exclusively relying on integral action for retrimming. These adaptive and reconfigurable flight control concepts are illustrated in the context of a fighter aircraft’s pitch plane dynamics. The novel adaptive and reconfigurable flight control system successfully handles a 50 per cent horiz
Platform: | Size: 2045952 | Author: zhouyang | Hits:

[AI-NN-PRUAV-Flight-Control-System

Description: :对某型无人机的飞行控制系统作了阐述,该飞行控制系统主要由飞行器分系统、测控与信息传输分系统、 任务设备分系统、地面支持分系统四大部分组成,飞行器分系统包括飞机机体、动力装置、导航与飞行控制、机上 电气设备及回收设备等;飞行控制技术的研究能使系统具有遥控、自主控制和应急返航能力.该无人机飞行控制系统已在某型无人机上得到应用,并已通过飞行试验验证,基本达到某型无人机的飞行控制要求.-: On a UAV' s flight control system were described, the aircraft flight control system consists of sub-systems, monitoring and information transmission subsystem, mission equipment subsystems, ground support subsystem four major components, vehicle sub-systems including airframe, power plant, navigation and flight control, aircraft equipment, electrical equipment and recycling flight control technology enables system with remote control, autonomous control and emergency return capability. The UAV flight control system has been applied on a UAV, and has been verified by flight test, basic to a UAV' s flight control requirements.
Platform: | Size: 388096 | Author: zhouyang | Hits:

[Other Embeded programflying-control

Description: 四轴飞行器非常详细的飞控源程序,内容相当丰富-Very detailed four-axis aircraft flight control source
Platform: | Size: 46080 | Author: 陆东杰 | Hits:

[VHDL-FPGA-VerilogInfrared-remote-control

Description: 用VERILOG语言实现的红外遥控实验,已成功用于实验用小飞机的飞行控制。-Experiment with infrared remote VERILOG language, has been successfully used in experiments with small aircraft flight control.
Platform: | Size: 719872 | Author: zyb | Hits:

[SCMG2553-flight-control

Description: MSP430G2553飞控说明 本程序由Arlyb编写!!! 程序说明: 为2014TI电赛开发! 配合MPU6050,可实现四轴飞行器姿态控制及其飞行控制,适合有一定基础的人!-MSP430G2553 flight control description The program is written by Arlyb!!! Description of the procedures: As the 2014TI game development! With the MPU6050, can realize four axis aircraft flight control and flight control, for those who have a certain basis!
Platform: | Size: 393216 | Author: 杨斌 | Hits:

[SCMF149-flight-control

Description: MSP430F149飞控说明 本程序由Arlyb编写!!! 程序说明: 配合MPU6050,可实现四轴飞行器姿态控制及其飞行控制,适合有一定基础的人!-MSP430F149 flight control description The program is written by Arlyb!!! Description of the procedures: With the MPU6050, can realize four axis aircraft flight control and flight control, for those who have a certain basis!
Platform: | Size: 673792 | Author: 杨斌 | Hits:

[OtherModel-aircraft-flight-control

Description: 以下是PID控制代码,我直接放在主函数里了 只用了PD控制,没加积分项。 MPU6050采样率设在200Hz,电调PWM频率也是200Hz-The following is a PID control code, I placed directly inside the main function Only a PD control, did not add the integral term. MPU6050 sampling rate set at 200Hz, the PWM frequency is 200Hz power transfer
Platform: | Size: 2048 | Author: 徐小波 | Hits:

[SCMFlight-Control-Source

Description: 飞控飞行器和遥控器源码,它是基于STM32F103CV6单片机的飞控源码-Aircraft flight control and remote control source code, which is based on SCM s flight control source STM32F103CV6
Platform: | Size: 7961600 | Author: 李柱 | Hits:

[Software EngineeringSTM32f405-four-axis-flight-control-

Description: STM32f405四轴飞控源代码内含MPU6050,MS5611,HMC5883L,GPS等驱动代码,还附有四轴飞行器的控制代码。- STM32f405 four-axis flight control source code contains MPU6050, MS5611, HMC5883L, GPS and other driver code, but also with four-axis aircraft control code.
Platform: | Size: 8009728 | Author: ljw | Hits:
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