GLIDER MODEL FLYING DYNAMICS SIMULATION EAGE-X ON LONGITUDINAL MATRA

IF 0.1 0 MUSIC
N. Retnowati, B. Junaidin, Engelbertus Rande
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引用次数: 0

Abstract

The Glider Eagle-X aircraft is an unmanned aircraft which is expected to fly with a height of 7 meters above the ground in Yogyakarta (120 m above sea level) with a flying speed of 10 m/s. In order for the Eagle-X glider to fly stably, it is necessary to analyze the flight stability of the Eagle-X glider model. Therefore, in this study, the analysis phase of static stability and dynamic response of disturbances in the longitudinal dimension was carried out. This can be useful for students so that they can better understand the analysis of static stability and dynamic response of disturbances in the longitudinal dimension. The results of the analysis show that the flight dynamics is a value of CM-α < 0 indicating the plane is statically longitudinal and the initial response of the graph is getting smaller which indicates the plane's motion is dynamically stable. The output of the stability analysis of the flying dynamics of the Eagle-X glider model is in the form of a graph. The simulation of the flying dynamics of the Eagle-X glider in the expected longitudinal dimension is shown by the aircraft movement following the graph from the results of the stability analysis which is used as the path of the Eagle-X glider model.
纵向矩阵上滑翔机模型飞行动力学仿真age - x
滑翔鹰- x飞机是一种无人驾驶飞机,预计将在日惹上空7米(海拔120米)以10米/秒的速度飞行。为了使Eagle-X滑翔机稳定飞行,有必要对Eagle-X滑翔机模型的飞行稳定性进行分析。因此,在本研究中,进行了纵向维度扰动的静稳定性和动态响应分析阶段。这可以帮助学生更好地理解纵向扰动的静稳定性和动态响应分析。分析结果表明,飞机的飞行动力学值为CM-α < 0,表明飞机是静纵向的,图形的初始响应越来越小,表明飞机的运动是动态稳定的。Eagle-X滑翔机模型飞行动力学稳定性分析的输出以图形形式表示。仿真Eagle-X滑翔机在期望纵向尺寸下的飞行动力学,用稳定性分析结果得出的飞机运动曲线图表示,该曲线图作为Eagle-X滑翔机模型的路径。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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