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某无人机基于载重任务的重心位置配置分析
引用本文:李永泽.某无人机基于载重任务的重心位置配置分析[J].科学技术与工程,2011,11(15):3472-3475.
作者姓名:李永泽
作者单位:西北工业大学航空学院,西安,710072
摘    要:基于某无人机的载重任务特点和要求,提出和分析了一种通过利用载重物调节无人机任务阶段重心位置,改善爬升和下滑阶段升阻特性来提高性能的方法。推导了重心位置变化与配平升力线斜率、升致阻力系数之间的关系。分析了通过调节重心位置改善爬升和下滑阶段升阻特性,从而提高性能的可行性;并结合实际模型进行了爬升与下滑阶段升阻特性计算。通过与任务阶段重心位置始终保持不变设计方案的对比,得出了通过调节重心位置可有效改善飞机爬升和下滑阶段升阻特性,提高性能的结论。

关 键 词:无人机  重心  配平升力  配平阻力  爬升率  下滑率
收稿时间:3/1/2011 10:05:44 PM
修稿时间:3/3/2011 10:24:33 AM

Analyze the C.G of a UAV Based on Load Task
liyongze.Analyze the C.G of a UAV Based on Load Task[J].Science Technology and Engineering,2011,11(15):3472-3475.
Authors:liyongze
Institution:LI Yong-ze,YUAN Chang-sheng,ZHANG Li(School of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,P.R.China)
Abstract:Based on the task features of a UAV's load mission requirements,it proposes and analyzes a way to improve the performance of UAV by using the physical load to adjust the c.g of the model aircraft during the mission phase.The climb and decline stages of lift-drag features is improved,and derived the relationship between trim lift induced drag and lift slope caused by the change of center of gravity.The feasibility of improving the lift-drag characteristics during climb and fell stage by adjusting the positio...
Keywords:UAV center of gravity trim lift trim drag rate of climb rate of down  
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