TY - GEN
T1 - Study of battery management for micro air vehicle power system
AU - Hu, Chun Hung
AU - Lai, Chia Hui
AU - Lin, Huang Chih
AU - Wang, Kuen Cheng
AU - Chen, Tsair Rong
PY - 2008/12/1
Y1 - 2008/12/1
N2 - Micro air vehicle has attracted significant attention on its potential application. This report studies the possible combination of selected available commercial batteries, propellers, motor, transmitter, receiver and electronic speed controller to provide maximum lift force under present restriction of micro air vehicle requirement. The possible combinations are suggested. All systems of unmanned aerial vehicle with strict limitation of weight and size must accomplish the mission in the conditions of low noise, long-range flight, and fast response. The requirement for accuracy is pretty restricted. This study explores the combination fulfilling the requirement, and utilizes power supply and micro components of transmit system available in the market to carry out optimal combination. We planned to select battery, motor, propeller, transmitter, receiver, and electrical transmission to carry out optimal combination to be used as power supply system of MAV (Micro Air Vehicle).
AB - Micro air vehicle has attracted significant attention on its potential application. This report studies the possible combination of selected available commercial batteries, propellers, motor, transmitter, receiver and electronic speed controller to provide maximum lift force under present restriction of micro air vehicle requirement. The possible combinations are suggested. All systems of unmanned aerial vehicle with strict limitation of weight and size must accomplish the mission in the conditions of low noise, long-range flight, and fast response. The requirement for accuracy is pretty restricted. This study explores the combination fulfilling the requirement, and utilizes power supply and micro components of transmit system available in the market to carry out optimal combination. We planned to select battery, motor, propeller, transmitter, receiver, and electrical transmission to carry out optimal combination to be used as power supply system of MAV (Micro Air Vehicle).
UR - http://www.scopus.com/inward/record.url?scp=84893194119&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84893194119&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84893194119
SN - 1934272434
SN - 9781934272435
T3 - IMETI 2008 - International Multi-Conference on Engineering and Technological Innovation, Proceedings
SP - 149
EP - 154
BT - IMETI 2008 - International Multi-Conference on Engineering and Technological Innovation, Proceedings
T2 - International Multi-Conference on Engineering and Technological Innovation, IMETI 2008
Y2 - 29 June 2008 through 2 July 2008
ER -