id	author	title	date	pages	extension	mime	words	sentence	flesch	summary	cache	txt
ajst-17385	Zhao, Haoyang	Classical PID Control of A Quadcopter UAV Under Variable Load Conditions	2024	3	.pdf	application/pdf	2014	69	54	The power model of UAV flight is established through MATLAB/Simulink, and the flight curves of two variable loads are demonstrated through the design, and the curves can intuitively detect the state of the UAV, and detect the stability of the UAV's fuselage in the case of variable load, which provides evidence for the stability of the UAV. Through experiments using UAV flight models it can be found that, the UAV can quickly adjust the flight state, so that it has been flying smoothly without losing control, which also proves that the model can be visualized to observe that the UAV will not affect the stability of the UAV's flight because of the changes in its own mass when it changes loads.	cache/ajst-17385.pdf	txt/ajst-17385.txt