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微小型无人驾驶直升机建模与仿真分析 被引量：1

Modeling and simulation of small-sized unmanned helicopter
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摘要 首先建立了微小型无人直升机较完整的动力学模型,然后利用参考文献提出的无人驾驶直升机自适应控制器,借助RealFlight模拟飞行软件对动力学模型和自适应控制算法进行了仿真。仿真结果表明,本文所建立的动力学模型与实际直升机的特性基本相符;自适应控制算法较好地控制了无人直升机的运动状态,表明该控制算法完全可以满足无人直升机控制的需要。 The authors mainly discussed the modeling and simulation of small - sized unmanned helicopter. They built a relatively integrated aerodynamic model for small - sized unmanned helicopter, and then performed a simulation for the dynamic model and an adaptive control arithmetic by using the adaptive controller for unmanned helicopters presented in the references and RealFlight R/C Flight Simulator, Helicopter was controlled well using the adaptive control arithmetic. The simulation results showed that the characteristics of the dynamic model were basically consistent with that of the real helicopter, and the adaptive control arithmetic could be used for implementing unmanned helicopter control.
作者 税海涛 王建文 李迅 马宏绪
机构地区 国防科技大学机电工程与自动化学院
出处 《电光与控制》 北大核心 2006年第3期49-53,共5页 Electronics Optics & Control
关键词 无人直升机 动力学模型 仿真 RealFlight unmanned helicopter dynamic model simulation RealFlight
分类号 V249.1 [航空宇航科学与技术—飞行器设计] TP273 [自动化与计算机技术—检测技术与自动化装置]
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参考文献7

二级参考文献15

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共引文献11

同被引文献10

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引证文献1

二级引证文献11

电光与控制
2006年 第3期

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