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 |
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Description: 模拟飞机爬升的仿真程序，可输出各种飞行姿态，很不错-Simulating an aircraft climb of the simulation program can output a variety of flight attitude, very good Platform: |
Size: 1024 |
Author:li jian |
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Description: 飞行器纵向回路姿态控制系统中阶跃干扰时定高平飞-Aircraft vertical loop attitude control system in step interference Gaoping set to fly Platform: |
Size: 8192 |
Author:duhaitao |
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Description: Trajectory and Attitude Plot
This function plot in the same figure the center trajectory and attitude of an aircraft. Platform: |
Size: 16384 |
Author:blue11 |
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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: 四旋翼飞行器姿态监控，通过上位机技术，可以帮助调试飞行器-Four-rotor aircraft attitude control, through the PC technology that can help debug aircraft Platform: |
Size: 4096 |
Author:gaofei |
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Description: 该程序包括了飞行器轨迹计算、陀螺和加速度计的采样输入、以及由四元素解算出的飞行器姿态、位置、速度-The program includes the aircraft trajectory calculation, the sampling gyro and accelerometer input, and the solution calculated by the four elements of aircraft attitude, position, velocity Platform: |
Size: 2048 |
Author:苏钰 |
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Description: 基于Dx9的飞机姿态控制程序，在pudn上找了很久都没找到，利用变换矩阵实现对飞机姿态的控制，对学习dx矩阵变换的朋友来说很有帮助。-Dx9-based aircraft attitude control program, look for a long time in pudn did not find, use the transformation matrix to achieve control of the aircraft attitude, learning dx matrix transformation friends helpful. Platform: |
Size: 923648 |
Author:Rong |
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Description: 捷联惯导航姿系统C语言实现，可以方便的得到飞机的飞行姿态。-Navigation position system SIMU program development, you can easily get the aircraft attitude. Platform: |
Size: 5120 |
Author:夏雷 |
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Description: This Program simulates "Attitude Indicator" of any aircraft. communication with serial port is not important for compiling and executing source code with Turbo C++. This program is good ideas for using mouse and 2D graphic, and has other learning subjects. Platform: |
Size: 9216 |
Author:Nasser |
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Description: 这个航空仪表控件是对飞机姿态数据的仪表显示控件.对于做地面站软件界面的朋友有很大的帮助.-The Aviation Instrument control instrumentation display controls for aircraft attitude data of great help for friends to do the ground station software interface. Platform: |
Size: 58368 |
Author:windofchina |
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Description: 通过调用OPENGL搭建飞机的三维模型，用外部姿态数据控制飞机姿态，实现逼真模拟。-Control external posture data through the three-dimensional model of call the OPENGL build aircraft, aircraft attitude to achieve a realistic simulation. Platform: |
Size: 413696 |
Author:冰叶西 |
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Description: 关于四轴飞行器姿态建模的资料。找了很辛苦，希望对大家有用。-Four aircraft attitude about modeling data. Looking very hard, we want to be useful. Platform: |
Size: 229376 |
Author:刘光明 |
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Description: 本文是前人总结的，关于四轴飞行器姿态解算的，我只是加以整理，方便阅读。-This paper is a summary of the previous, about four axis aircraft attitude solution, I just tidying up, easy to read. Platform: |
Size: 330752 |
Author:suyan |
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Description: 基于apm2.5的飞行器姿态角计算及输出 以及 GPS 高度 经纬度输出 -Calculated based aircraft attitude angle and height of the output and GPS latitude and longitude of the output apm2.5 Platform: |
Size: 992256 |
Author:weno |
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