1925.
Autopilots for Ultra Lightweight Robotic Birds: Automatic Altitude Control and System Integration of a Sub-10 g Weight Flapping-Wing Micro Air Vehicle
蕭富元; Hsiao, Fu-Yuen; Yang, Lung-Jieh; 楊龍杰; Lin, Sen-Huang; Chen, Cheng-Lin; Shen, Jeng-Fu
,
2012-10
[Graduate Institute & Department of Aerospace Engineering] Journal Article, [Graduate Institute & Department of Mechanical and Electro-Mechanical Engineering] Journal Article IEEE Control Systems Magazine 32(5), p.35-48
if the computational speed
meats the real-time reqiirements, an MAV is highly con-
strained by size and weight restrictiins. Consequently,
when
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