Micro air vehicle: Architecture and implementation

Huai-Yu Wu; Dong Sun; Zhao-Ying Zhou; Shen-Shu Xiong; Xiao-Hao Wang

doi:10.1109/ROBOT.2003.1241649

Micro air vehicle: Architecture and implementation

Huai-Yu Wu
, Dong Sun
, Zhao-Ying Zhou
, Shen-Shu Xiong
, Xiao-Hao Wang

Research output: Journal Publications and Reviews › RGC 22 - Publication in policy or professional journal

7 Citations (Scopus)

Abstract

This paper presents the development of an electrically powered Micro Air Vehicle (MAV) with a wingspan of 360 mm. A miniature flight control system including a self-made micro video image system especially suitable for MAV is developed. The aerodynamic performance of several airfoil sections at low chord Reynolds numbers is analyzed in order to find an optimum airfoil section for the MAV prototype. A small-sized propulsion testing setup is built to measure the performance of the motor-gear-propeller-battery combination so that an efficient propulsion system can be obtained. The TH360 MAV with a payload of a self-made micro color video image system has been successfully tested in the real-time flight, where the real-time images of the ground target can be transmitted from the onboard video camera to the ground.

Original language	English
Pages (from-to)	534-539
Journal	Proceedings - IEEE International Conference on Robotics and Automation
Volume	1
DOIs	https://doi.org/10.1109/ROBOT.2003.1241649
Publication status	Published - 2003
Event	2003 IEEE International Conference on Robotics and Automation - The Grand Hotel, Taipei, Taiwan, China Duration: 14 Sept 2003 → 19 Sept 2003 https://ieeexplore.ieee.org/xpl/conhome/8794/proceeding

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title = "Micro air vehicle: Architecture and implementation",

abstract = "This paper presents the development of an electrically powered Micro Air Vehicle (MAV) with a wingspan of 360 mm. A miniature flight control system including a self-made micro video image system especially suitable for MAV is developed. The aerodynamic performance of several airfoil sections at low chord Reynolds numbers is analyzed in order to find an optimum airfoil section for the MAV prototype. A small-sized propulsion testing setup is built to measure the performance of the motor-gear-propeller-battery combination so that an efficient propulsion system can be obtained. The TH360 MAV with a payload of a self-made micro color video image system has been successfully tested in the real-time flight, where the real-time images of the ground target can be transmitted from the onboard video camera to the ground.",

author = "Huai-Yu Wu and Dong Sun and Zhao-Ying Zhou and Shen-Shu Xiong and Xiao-Hao Wang",

year = "2003",

doi = "10.1109/ROBOT.2003.1241649",

language = "English",

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pages = "534--539",

journal = "Proceedings - IEEE International Conference on Robotics and Automation",

issn = "1050-4729",

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note = "2003 IEEE International Conference on Robotics and Automation ; Conference date: 14-09-2003 Through 19-09-2003",

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TY - JOUR

T1 - Micro air vehicle

T2 - 2003 IEEE International Conference on Robotics and Automation

AU - Wu, Huai-Yu

AU - Sun, Dong

AU - Zhou, Zhao-Ying

AU - Xiong, Shen-Shu

AU - Wang, Xiao-Hao

PY - 2003

Y1 - 2003

N2 - This paper presents the development of an electrically powered Micro Air Vehicle (MAV) with a wingspan of 360 mm. A miniature flight control system including a self-made micro video image system especially suitable for MAV is developed. The aerodynamic performance of several airfoil sections at low chord Reynolds numbers is analyzed in order to find an optimum airfoil section for the MAV prototype. A small-sized propulsion testing setup is built to measure the performance of the motor-gear-propeller-battery combination so that an efficient propulsion system can be obtained. The TH360 MAV with a payload of a self-made micro color video image system has been successfully tested in the real-time flight, where the real-time images of the ground target can be transmitted from the onboard video camera to the ground.

AB - This paper presents the development of an electrically powered Micro Air Vehicle (MAV) with a wingspan of 360 mm. A miniature flight control system including a self-made micro video image system especially suitable for MAV is developed. The aerodynamic performance of several airfoil sections at low chord Reynolds numbers is analyzed in order to find an optimum airfoil section for the MAV prototype. A small-sized propulsion testing setup is built to measure the performance of the motor-gear-propeller-battery combination so that an efficient propulsion system can be obtained. The TH360 MAV with a payload of a self-made micro color video image system has been successfully tested in the real-time flight, where the real-time images of the ground target can be transmitted from the onboard video camera to the ground.

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U2 - 10.1109/ROBOT.2003.1241649

DO - 10.1109/ROBOT.2003.1241649

M3 - RGC 22 - Publication in policy or professional journal

SN - 1050-4729

VL - 1

SP - 534

EP - 539

JO - Proceedings - IEEE International Conference on Robotics and Automation

JF - Proceedings - IEEE International Conference on Robotics and Automation

Y2 - 14 September 2003 through 19 September 2003

ER -

Micro air vehicle: Architecture and implementation

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