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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: 278096 | Author: jake | Hits:

[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:

[ARM-PowerPC-ColdFire-MIPSarm_auto_plane

Description: 自动驾驶仪是无人机飞行控制系统的核心,采用ARM 处理器和MEMS传感器件设计小型无人机自动驾驶仪符合飞 控系统的高精度、小型化、数字化发展趋势,具有很好的应用 前景。-Autopilot UAV flight control system is the core of the use of ARM processors and MEMS sensor design small UAV autopilot flight control system in line with the high-precision, miniaturization, digitalization trend of development, has good application prospects .
Platform: | Size: 530432 | Author: pengjun | Hits:

[Windows DevelopF16FlightControlSimulation

Description: 经典的F16飞行控制仿真程序,做飞行控制的朋友们一起来探讨吧-Classic F16 flight control simulation program, to do flight control one of my friends together to explore it
Platform: | Size: 199680 | Author: 钱伟 | Hits:

[transportation applicationsfdc13.ZIP

Description: MATLAB在飞行动力学和控制中应用的工具-MATLAB in the flight dynamics and control application tool
Platform: | Size: 765952 | Author: 吴军 | Hits:

[matlabdubsi10-2

Description: 飞机仿真软件包dubsi10-2,可以与FDC tool(本站已有)一起使用的matlab/simulink仿真软件,主要对飞机的滚转姿态控制进行仿真研究,内有丰富的案例。-The Dutchroll Blockset for Simulink, DUBSI, is a stand-alone version of the blocklibrary BLOCKLIB_MISC in version 2.0 (or later) of the Flight Dynamics and Control (FDC) Toolbox, which is currently under development. It contains a number of general-purpose Simulink blocks, which can be used for more applications than flight dynamics research only. Both the FDC toolbox and the DUBSI blockset are copyrighted by M.O. Rauw see COPYING.TXT for more details.
Platform: | Size: 225280 | Author: lili | Hits:

[matlabwork

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 | Hits:

[matlabrandControl

Description: 飞机飞行仿真中,对四个主要控制量,包括油门、升降舵、副翼及方向舵控制,分别提供持续2秒的随机大小的阶跃控制输入,四个控制量互相独立。可以用于飞行动力学系统辨识、参数识别等。-Flight simulation, the four main control volume, including throttle, elevator, aileron and rudder control, to provide for 2 seconds, respectively, a random step size control inputs, four control variables independent of each other. Can be used in flight dynamics system identification, parameter identification.
Platform: | Size: 1024 | Author: dongniue | Hits:

[matlabnon-controlled--missile-Simulation

Description: 用matlab/simulink搭建的六自由度无控弹道导弹模型,用来仿真在不加控制力作用下弹道导弹的飞行轨迹,simulink模型用RTW很方便转换成c/c++,适合飞行控制专业的新手学习,有问题请留言。-Using matlab/simulink to build the six degrees of freedom without controlled ballistic missile model is used to simulate the flight trajectory, in uncontrolled force of ballistic missile flight control, suitable for beginners to professional learning, have any questions please leave a message.
Platform: | Size: 25600 | Author: 周胜俞 | Hits:

[Software Engineeringyijidaolibai

Description: 单级倒立摆的模糊控制以及在MATLAB中的仿真倒立摆在研究双足机器人直立行走、火箭发射过程的姿态调整和直升机飞行控制领域中有重要的现实意义,相关的科研成果己经应用到航天科技和机器人学等诸多领域-A handstand on the study of bipedal robot to walk upright, rocket launch posture adjustment and in the field of helicopter flight control have important realistic meaning, related research achievement has been applied to many fields such as aerospace science and technology and robotics
Platform: | Size: 578560 | Author: 爪瓦 | Hits:

[matlabUAVControl_PID

Description: 无人飞行器飞行控制仿真程序,通过MATLAB中的Simulink模块进行无人飞行器的动力学模型搭建进行无人机飞行仿真。-Kinetic model of UAV flight control simulation program, carried out by unmanned aircraft in MATLAB Simulink modules were built UAV flight simulation.
Platform: | Size: 613376 | Author: 谢亚恩 | Hits:

[matlabkengbun_v22

Description: MIMO OFDM matlab仿真,采用加权网络中节点强度和权重都是幂率分布的模型,包含飞行器飞行中的姿态控制,如侧滑角,倾斜角,滚转角,俯仰角。- MIMO OFDM matlab simulation, Using weighted model nodes in the network strength and weight are power law distribution, It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle.
Platform: | Size: 4096 | Author: 李青龙 | Hits:

[Otherhanjen_v83

Description: 包含飞行器飞行中的姿态控制,如侧滑角,倾斜角,滚转角,俯仰角,采用了小波去噪的思想,内含心电信号数据及运用MATLAB写的源代码。- It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle, Using wavelet denoising thought, ECG data and includes source code written in MATLAB.
Platform: | Size: 5120 | Author: 张海军 | Hits:

[matlabfuigao_v58

Description: 在matlab R2009b调试通过,matlab编写的元胞自动机,包含飞行器飞行中的姿态控制,如侧滑角,倾斜角,滚转角,俯仰角。- In matlab R2009b debugging through, matlab prepared cellular automata, It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle.
Platform: | Size: 5120 | Author: 王正 | Hits:

[matlabsrbjdkuc

Description: MIMO OFDM matlab仿真,采用加权网络中节点强度和权重都是幂率分布的模型,包含飞行器飞行中的姿态控制,如侧滑角,倾斜角,滚转角,俯仰角。 - MIMO OFDM matlab simulation, Using weighted model nodes in the network strength and weight are power law distribution, It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle.
Platform: | Size: 6144 | Author: 侯海 | Hits:

[Algorithmnentou

Description: 内含心电信号数据及运用MATLAB写的源代码,多抽样率信号处理,包含飞行器飞行中的姿态控制,如侧滑角,倾斜角,滚转角,俯仰角。- ECG data and includes source code written in MATLAB, Multirate signal processing, It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle.
Platform: | Size: 6144 | Author: 苏耀鹏 | Hits:

[matlabpingpui_v49

Description: 现代信号处理中谱估计在matlab中的使用,Pisarenko谐波分解算法,包含飞行器飞行中的姿态控制,如侧滑角,倾斜角,滚转角,俯仰角。- Modern signal processing used in the spectral estimation in matlab, Pisarenko harmonic decomposition algorithm, It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle.
Platform: | Size: 5120 | Author: 王煜娜 | Hits:

[matlabhengjun_V8.4

Description: 内含心电信号数据及运用MATLAB写的源代码,基于小波变换的数字水印算法matlab代码,包含飞行器飞行中的姿态控制,如侧滑角,倾斜角,滚转角,俯仰角。- ECG data and includes source code written in MATLAB, Based on wavelet transform digital watermarking algorithm matlab code, It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle.
Platform: | Size: 5120 | Author: yangjenqen | Hits:

[matlabfaigeng_v48

Description: 包含飞行器飞行中的姿态控制,如侧滑角,倾斜角,滚转角,俯仰角,现代信号处理中谱估计在matlab中的使用,数值分析的EULER法。- It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle, Modern signal processing used in the spectral estimation in matlab, EULER numerical analysis method.
Platform: | Size: 4096 | Author: qeihankeifao | Hits:

[mathematica无人机飞控代码

Description: MATLAB无人家飞控代码,有需要的可以下载(MATLAB without somebody else's flight control code, can be downloaded in need)
Platform: | Size: 86016 | Author: 1090072370 | Hits:
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