System Identification of Small UAVs with MEMS-based Avionics

System Identification of Small UAVs with MEMS-based Avionics
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采用基于 MEMS 的航空电子设备的小型无人机系统识别

DOI：
10.2514/6.2009-1907
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发表时间：
2009
期刊：
--
影响因子：
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通讯作者：
Shinji Suzuki
Shinji Suzuki
中科院分区：
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文献类型：
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作者：
M. Naruoka;T. Hino;R. Nakagawa;T. Tsuchiya;Shinji Suzuki

文献摘要

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针对目前小型无人机系统辨识主要依赖风洞试验的现状，提出了一种基于MEMS技术的小型、轻型、低成本航空电子设备。航空电子设备能够准确地收集导航、风和控制输入数据。以某小型无人机为例进行了飞行试验，利用航电和系统辨识技术获得的飞行数据，准确地获得了该无人机的纵向稳定导数。
A new MEMS-based small, light, and cost-effective avionics is proposed in order to improve the current situation of system identification of small unmanned aerial vehicles (UAVs), which mostly depends on difficult wind tunnel tests. The avionics is capable of gathering navigation, wind, and control input data accurately. Flight tests with a small UAV are conducted, and its longitudinal stability derivatives are obtained accurately using flight data obtained by the avionics and system identification techniques.