中文说明：无人机的动力学仿真建模与姿态控制的matlab ，在对小型四旋翼无人机位姿控制研究时，为了缩短研究周期和研究费用，对该系统进行建模研究，并对其进行仿真分析．由于悬停模式是飞行器的最基本和最关键的飞行姿态，本文基于悬停模式迸行建模，并基于近似扰动观点建立模型的状态空间方程，在Matlab／Sim-ulink平台上，对模型的悬停模式进行了PID控制仿真
English Description：
Dynamic simulation modeling and attitude control of UAV Based on MATLAB In order to shorten the research period and cost, the system is modeled and simulated. Because hovering mode is the most basic and critical flight attitude of the aircraft, this paper establishes the model based on hovering mode and the state space equation of the model based on the viewpoint of approximate disturbance On the im ULINK platform, the PID control simulation of the hovering mode of the model is carried out