Description: 一个飞机调度员模拟训练程序,可以添加跑道数量,控制飞机飞行的速度.默认的密码可以在AtcSystem类里面修改,其中内置了三个用户名.这套系统是我和几个国外同学合力开发的,希望对大家有帮助-an aircraft dispatcher simulation training procedures, the number can be added the runway, control aircraft flying speed. The default password can AtcSystem categories changes with a built-in the three user. This system is my classmates and several foreign development efforts, we hope to help Platform: |
Size: 166659 |
Author:liushuoling |
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Description: 一个飞机调度员模拟训练程序,可以添加跑道数量,控制飞机飞行的速度.默认的密码可以在AtcSystem类里面修改,其中内置了三个用户名.这套系统是我和几个国外同学合力开发的,希望对大家有帮助-an aircraft dispatcher simulation training procedures, the number can be added the runway, control aircraft flying speed. The default password can AtcSystem categories changes with a built-in the three user. This system is my classmates and several foreign development efforts, we hope to help Platform: |
Size: 165888 |
Author:liushuoling |
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Description: 我自己编写的飞行器控制系统设计代码，使用的线性不等式的方法。看m文件说明，最后还有simlunk模型仿真。-I have written an aircraft control system design code, the use of the linear inequality method. M document describes the look, and last but not simlunk model simulation. Platform: |
Size: 11264 |
Author:jesse |
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Description: 飞行器惯性导航控制系统设计仿真平台实现方案-Aircraft inertial navigation control system design and simulation platform for the realization of the program Platform: |
Size: 787456 |
Author:jingpengyu |
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Description: 用LabVIEW实现的“飞行姿态控制仿真”。内有vi：俯仰和滚转控制器、航向控制器、键按下增大、键盘操作、姿态角误差转换、阻尼器。还有9个显示vi和12个模型vi。
飞行控制的目的主要是通过控制飞行器的姿态和轨迹来完成飞行任务，然而飞行轨迹很大程度由飞行姿态决定。可见飞行器姿态控制，在整个飞行控制系统中处于重中之重的地位。飞行姿态控制的好坏直接关系到飞机能否安全、平稳、快速的地飞行。与其它控制系统一样，可用稳定性和动稳态性能来衡量控制效果。稳态时，要使飞行器姿态足够接近所需的飞行姿态，才能让飞机以一定的航迹航行。而姿态变化的过程，要求系统稳定，响应快，超调小，振荡少，即姿态能够快速平稳过渡。早期，可以通过优化飞机的气动布局来改良飞机的飞行性能，但随着飞行的速度与高度的增加，空气变得稀薄，阻尼随之减小，飞行的气动模型也发生了大的改变，已经难以通过外形设计来增强稳定性，而设计优良飞行姿态控制器是必由之路.
-Using LabVIEW to achieve the "flight attitude control simulation." There vi: pitch and roll control, heading control, key press increases, keyboard operation, attitude angle error change, and the dampers. There are nine show vi and 12 model vi.
The main purpose of the flight control is by controlling the aircraft attitude and flight trajectory to complete the task, but a large degree trajectory decision by the flight attitude. Spacecraft attitude control can be seen in the flight control system in the most important position. Flight attitude control has direct bearing on whether the aircraft safe, stable, fast to the ground. And other control systems, stability and dynamic steady-state performance can be measured in control performance. Steady state, make the aircraft attitude close enough to the required flight attitude, to allow the aircraft to a certain track navigation. The attitude change process, requiring system stability, fast response, small overshoot, small oscillations, Platform: |
Size: 424960 |
Author:zhou |
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Description: The Spacecraft Control Toolbox is composed of MATLAB m-fi les and mat-fi les, organized into a set of modules by subject. It is essentially a library of functions for analyzing spacecraft and missions. There is a substantial set of
software which the Spacecraft Control Toolbox shares with the Aircraft Control Toolbox, and this software is in a module called Common. The core spacecraft fi les are in SC and SCPro along with special plotting tools in Plotting.
The new CubeSat module demonstrates mission planning and simulation for nanosatellites. These fi ve modules are referred to together as the Core toolbox. Functions for estimation, orbit analysis, subsystem analysis, and detailed
attitude control system examples are grouped in separate modules. All of the modules are described in the following table, including the add-on modules which are purchased separately. Platform: |
Size: 9728000 |
Author:Huy |
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Description: 抄录的是飞行器制导与控制及其matlab仿真技术
毕开波编著p159，仿真的是二维比例导引仿真，递推采用的是龙哥库塔方法
用的不是欧拉方法
我花了很长时间才敲到电脑上，望大家给点掌声，打字员llittlebird
错误的没有，有图为证
要下载两个-Reproduces the Aircraft Guidance and Control of matlab simulation Bi Kaibo ed p159, the simulation is two-dimensional proportional navigation simulation, recursive method used in the Long Ge Kuta Euler method is not used for a long time I spent knocking to the computer, hope everyone to the point of applause, typists llittlebird mistake not, there are two photo cards to download Platform: |
Size: 4096 |
Author:zhang |
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Description: 飞行器全包线控制律算法实现及仿真Aircraft full envelope control law and simulation algorithm-Aircraft full envelope control law and simulation algorithm Platform: |
Size: 454656 |
Author:fly2345 |
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Description: 根据航母海上运动具有平稳随机过程的特点，利用功率谱模型对其进行建
模，尽可能真实地反映航母的运动状况。分析甲板运动带来的理想着舰点的变化，针对舰载机飞行高度进行模糊控制。按照舰载机自动着舰控制系统的大致结构，从内而外依次对自动飞行控制系统、进场功率补偿系统、甲板运动补偿器进行了研究和设计，在Matlab中对其进行完整建模，并通过仿真加以验证。设计模糊PID控制器，利用模糊控制系统对控制器参数进行在线调整，最后通过Matlab仿真，验证该方法可以有效改进舰载机的着舰品质。-According to the aircraft carrier Marine sport has stable random process characteristics, the use of power spectrum model on the modeling, as a true reflection of carriers movement status. Analysis of the deck movement to bring the ship to point ideal for change, the flying height carrier-borne machine fuzzy control. According to the ship carrier-borne machine automatic control system, the general structure of automatic order from inside and outside the flight control system, approach power compensation system, deck sports compensator was studied and design, the in Matlab simulation modeling and complete verified. Design fuzzy PID controller by using fuzzy control system, the controller parameters for online adjustment, the last through Matlab simulation show that the method can effectively improve the quality of the ship carrier-borne machine. Platform: |
Size: 55296 |
Author:占新 |
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Description: F16飞机纵向控制增稳系统仿真模型，解压缩后在matlab2006b以上版本使用。先运行SAS_lon_4ord_ini.m进行初始化，再运行SAS_lon_4ord.mdl。可以修改反馈参数。-F16 aircraft longitudinal control augmentation system simulation model, unzip and use it in matlab2006b. Run SAS_lon_4ord_ini.m first for initialion, and then run SAS_lon_4ord.mdl. You can modify the feedback parameters. Platform: |
Size: 8192 |
Author:liu xingyu |
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Description: 自己编的的弹道仿真程序，希望能对学飞行器控制的人有些帮助。-Own series of trajectory simulation program, hoping to learn some people to help aircraft control. Platform: |
Size: 10353664 |
Author:朱永丽 |
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Description: 本 文 深 入研究了开发三维飞行仿真系统的关键技术。主要研究了视景仿真技术、动
画生成技术和DirectX 技术，对当前常用的三种视景仿真软件进行了功能比较。重点介
绍了该系统采用的用于游戏和交互式多媒体开发的DirctX 技术。在window sXP系统
环境下，基于计算机可视化仿真技术，利用可视化程序开发工具软件VB6.0及应用程序
编程接口DiretX，建立了一个具有人机交互功能的X型遥控模拟飞机三维飞行仿真系
统。生成了能够使操纵手产生身临其境感觉的交互式仿真环境，实现了操纵手与该环境
之间的自然交互。系统构造了逼真的三维模型，并且为其制作了逼真的纹理，逼真地模
拟了x型遥控模拟飞机飞行的真实情况。系统模拟了一架X型遥控模拟飞机在一个地
形上空的飞行过程，可以使用键盘对飞机模型进行控制，模拟飞机的俯仰、左卡、右卡、
回收等操作，以实现对实际飞行操控的模拟仿真训练。利用该系统进行模拟训练结束后，
系统还可以根据操纵手的操纵情况评出操作成绩，对操纵手的操纵水平进行客观的评
估。-This article studies the key technologies for the development of three-dimensional flight simulation system. Mainly to study the visual simulation technology, dynamic
The painting generated and DirectX technology, the current three commonly used visual simulation software feature comparison. Focus on referrals
The system used for games and interactive multimedia development DirctX. In the window sXP system
Environment, computer-based visual simulation technology, the use of visual application development tool software VB6.0 application
The programming interface DiretX, a human-computer interaction X-type remote control three-dimensional simulation of aircraft flight simulation system
Systems. Generate interactive simulation environment that enables the manipulator hand immersive feeling manipulator hand with the environment
Between natural interaction. System to construct a realistic three-dimensional model, and its production of realistic textures, realistic mode
Intends x remo Platform: |
Size: 2321408 |
Author:caowenming8 |
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Description: 用欧拉角表示的飞行器姿态运动学方程在大角度时会出现奇异现象,而采用四元数来
表示,则可以避免这个问题。因此,飞行器运动学方程都采用四元数来表示。而飞行器的控
制规律都采用欧拉角来表示,且欧拉角表示姿态角比起四元数更加形象,更易于被人理解,
所以,在飞行器控制系统仿真设计的时候,需要四元数与欧拉角之间的转换。给定1 个欧拉
角,对应1 个四元数,因而欧拉角到四元数之间这种一一对应的关系使得欧拉角到四元数的
转换比较容易。但是,1 个四元数通常有1 个或者2 个欧拉角与之对应,它们之间不是一一
的对应关系,因而,四元数到欧拉角之间的转换比较困难。一般文献或者参考资料上的转换
仅仅适于欧拉角在- 90°～ + 90°之间的情况[1 ] 。文献[ 2 ,3 ]中给出了滚动轴在- 90°～ + 90°
之间变化,俯仰轴、偏航轴在- 180°～ + 180°之间变化的四元数到欧拉角的转换公式。本文
提出了滚动、俯仰和偏航3 个轴的欧拉角均在- 180°～ + 180°之间取值的全角度转换算法,
经过数字仿真证实,这个算法是完全正确的、而且很实用。-Euler angles of the spacecraft attitude kinematics equation at large angles appear strange phenomenon, and quaternion
, You can avoid this problem. Therefore, the aircraft kinematic equations using quaternion to represent. Aircraft control
The system of law Euler angles and Euler angles attitude angle than the the quaternion more image easier to be understood,
Therefore, in the design of aircraft control system simulation, you need to convert between quaternions and Euler angles. Given an Euler
Angle corresponding to a quaternion, which this one-to-one relationship between the Euler angles to quaternion makes Euler angles to quaternion
Conversion is relatively easy. However, a quaternion usually have one or two corresponding Euler angles between them than eleven
The correspondence relationship, therefore, the quaternion to convert between the Euler angle is relatively difficult. General literature or reference conversion
Only suitable for Euler angles- 90 ° to+ 90 ° betwe Platform: |
Size: 2048 |
Author:yang |
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Description: 用matlab/m文件编写的计算标准大气压小程序，非常实用，可以用于各种飞行器控制设计等方面的仿真，m文件编写很容易转换成c/c++，有问题请留言。-Written using matlab/m file calculation standard atmospheric pressure of small procedures, very useful, can be used for simulation of various aircraft control design, m document can be easily converted into c/c++, have any questions please leave a message Platform: |
Size: 1024 |
Author:周胜俞 |
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Description: 关于飞行器制导控制方面比较全面的仿真源代码，其中包括飞行器三自由度和六自由度仿真，单次仿真和蒙特卡洛仿真，EKF算法和UKF算法仿真等等。-On aircraft guidance control more comprehensive simulation source code, including aircraft and six degrees of freedom simulation of three degrees of freedom, a single simulation and Monte Carlo simulation, EKF and UKF algorithm simulation algorithms and so on. Platform: |
Size: 310272 |
Author:周池军 |
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Description: 基于matlab以及simulink，开发出飞行器控制的六自由度方程式，并且建立了飞机的执行机构和PID控制率的全仿真模型(Based on matlab and simulink, the six degree of freedom equation of aircraft control is developed, and the full simulation model of aircraft's actuator and PID control rate is established) Platform: |
Size: 5286912 |
Author:冒泡的雨 |
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