搜索资源列表
AtmosphericSpaceFlightDynamics
- 航空器飞行器动力学模型，可以看看，挺好的-AtmosphericSpace Flight Dynamics
FlightDynamicsofaCessna
- 卡西尼飞行器飞行动力学模型，挺好的，航天专业的可以-FlightDynamicsofaCessna
DOF2
- 编写的模型飞机控制模型和六自由度模型。根据《航空飞行器飞行动力学》书中的公式编写。-The preparation of the model aircraft control model and six degrees of freedom model. According to " air vehicle flight dynamics" formula for writing the book.
flightgear
- 将飞行仿真系统分解为飞行器动力学模型与飞控系统、仪表显示及操纵控制台、视景仿真等独立子系统, 并以FlightGear 和Matlab/Simulink为平台设计搭建一套分布式飞行仿真系统。-The decomposition of the flight simulation system for the vehicle dynamics model and flight control systems, instrument display and manipulation of the
aeroblk6dofbody
- 航空飞行器6自由度动力学模型，用于飞行力学和飞机控制仿真-Aviation aircraft 6 DOF dynamics model for flight mechanics and aircraft control simulation
aeroblk_airframe
- 飞行器纵向3自由度非线性动力学模型的线性化-Aircraft vertical 3-DOF nonlinear dynamic model linearization
Flexibleaircraft_SMC
- 基于滑模变结构理论的柔性飞行器姿态控制仿真程序，通过利用Matlab下的S-function模块分别描述柔性飞行器姿态动力学模型和滑模变结构控制策略实现系统仿真。-An simulation model of flexible aircraft under sliding mode control is realized by means of s-function method of Matlab.
Modeling-of-trajectory
- Matlab进行再入式飞行器轨道建模与仿真，建立各种模型，最后获得飞行器的动力学模型，并调用龙格库塔函数求解该微分方程初值问题。-Matlab for reentry spacecraft orbit modeling and simulation, the establishment of various models, and finally obtain the dynamic model of the aircraft, and call the Runge-Kutta function
quadrotor-simm
- 自己做的基于非线性动力学模型的四旋翼飞行器用的PID控制的姿态控制仿真模型和位置回路的仿真模型，inversion1是给定位置解算姿态的文件-Based on their own four-rotor aircraft nonlinear dynamic model with attitude control PID control simulation model simulation model and the position loop, inversion1 a given locati
UAVControl_PID
- 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.
four-rotor-aircraft
- 关于飞行器的研究，建立四旋翼飞行器基于刚体的初步力学模型，及参数测量，研究多旋翼飞行器的空气动力学特性。基于模型的控制算法。-Research on the aircraft, the establishment of four-rotor aircraft based on preliminary mechanical model of a rigid body, and parameter measurement, Multi-rotor aerodynamics. Model-based
AIRCRAFT
- 建立了四旋翼飞行器悬停姿态动力学模型，并进行了仿真分析，在开环控制的前提下分析了结构增稳和橡筋阻尼方法对飞行器平台姿态定性的影响，并提出了一种开环控制下实现稳定悬停的策略。-The establishment of a four-rotor aircraft hovering attitude dynamics model and simulation analysis, under the premise of open-loop control analyzes the impact of
Slide
- 北航与慕尼黑工业大学 飞行器课件 讲解四轴飞行器的空气动力学模型，位姿控制PID -Northern Technical University of Munich and courseware to explain Quadcopter aircraft aerodynamic model, pose PID control
仿真
- 四旋翼无人机的动力学模型建模验证分析，模拟运行飞行器的飞行过程。(Four, the dynamic model of rotor UAV is modeled and analyzed to simulate the flight process of the running aircraft.)
gaodu
- 四旋翼无人机是一种具有六个自由度和四个输入的欠驱动强耦合、外型新颖结构简单的飞行器。由于其具有制造成本地、重量轻、体积小、操作简单、使用方便、隐身性好、对作战环境要求低的特点，使其能准确、高效的执行各种军事或民用任务，因此四旋翼无人机具有一定的军事和民用价值。本课题针对四旋翼无人机的特点和飞行原理，对其动力学分析以及运动控制的研究，利用牛顿—欧拉方程，建立了四旋翼无人机的动力学模型,并针对该模型设计了PID四通道控制系统,且在Matlab/Simulink仿真平台上,利用PID控制系统对四旋翼无