NDLI: A control system for pitch attitude control investigation of insect inspired MAV

Content Provider	IEEE Xplore Digital Library
Author	Meijun Hu XingYao Yan Lingjuan Mu
Copyright Year	2011
Description	Author affiliation: College of Metrology Technology and Engineering, China Jiliang University, Hangzhou, China (XingYao Yan) \|\| Engineering Center, China Jiliang University, Hangzhou, China (Lingjuan Mu) \|\| Fair Friend Institute of Electro-Mechanics Hangzhou Vocational and Technical College, China (Meijun Hu)
Abstract	To study the pitch attitude control method of a man made insect inspired micro aero vehicle (IIMAV) model in a micro wind tunnel dynamically, the pitch attitude of the IIMAV need to be adjusted instantaneously according to the moments measured by a six dimensional micro force sensor which was mounted under the body of IIMAV model, this gives rise the design of this control system. An enhanced STC micro processor was taken as the centre process unite of the whole circuit, and serial peripheral interface (SPI) was used to communicate with the micro six dimensional force sensor to get data, and a regulation resistance together with an analog to digital converter circuit were used to get real pitch attitude of the IIMAV. Step motor was used to drive the model to target pitch attitude angle dynamically according to the moment measured by the micro sensor, and PID algorithm was taken in the feedback control loop of pitch angular velocity, which improves the accuracy of pitch angular velocity greatly.
Starting Page	562
Ending Page	565
File Size	104369
Page Count	4
File Format	PDF
ISBN	9781424487271
e-ISBN	9781424487288
DOI	10.1109/CSAE.2011.5952741
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2011-06-10
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Resistance MAVs Attitude control Insects Wind tunnel Introduction Aerodynamics Insect inspired Force sensors Velocity measurement Aircraft Pitch attitude
Content Type	Text
Resource Type	Article

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