TY - GEN
T1 - Design of the flight control system for a small-scale helicopter
AU - Du, Yu Hu
AU - Fang, Jian Cheng
PY - 2013
Y1 - 2013
N2 - Compared with the fixed-wing aerial vehicles, small-scale unmanned helicopter (SUH) has the advantages of taking off and landing vertically, cruising under ultra low speed, and sustained hovering in the air. SUH has properties of nonlinear, unstable, strongly coupling, and applying control system for SUH is considered as a challenging task. This paper presents the design of the flight control system for a SUH. This flight control system consists of two parts, namely, ground station and onboard part. Various experiments have been conducted to test the performance of this flight control system, and some of the results are presented at the end.
AB - Compared with the fixed-wing aerial vehicles, small-scale unmanned helicopter (SUH) has the advantages of taking off and landing vertically, cruising under ultra low speed, and sustained hovering in the air. SUH has properties of nonlinear, unstable, strongly coupling, and applying control system for SUH is considered as a challenging task. This paper presents the design of the flight control system for a SUH. This flight control system consists of two parts, namely, ground station and onboard part. Various experiments have been conducted to test the performance of this flight control system, and some of the results are presented at the end.
KW - Aerial vehicles
KW - Flight control system
KW - Small-scale unmanned helicopter
UR - https://www.scopus.com/pages/publications/84884841628
U2 - 10.4028/www.scientific.net/AMM.380-384.459
DO - 10.4028/www.scientific.net/AMM.380-384.459
M3 - 会议稿件
AN - SCOPUS:84884841628
SN - 9783037858202
T3 - Applied Mechanics and Materials
SP - 459
EP - 462
BT - Vehicle, Mechatronics and Information Technologies
T2 - 2013 International Conference on Vehicle and Mechanical Engineering and Information Technology, VMEIT 2013
Y2 - 17 August 2013 through 18 August 2013
ER -