TY - GEN
T1 - Modeling and attitude control of Bi-copter
AU - Zhang, Qimin
AU - Liu, Zihe
AU - Zhao, Jieru
AU - Zhang, Shuguang
N1 - Publisher Copyright:
© 2016 IEEE.
PY - 2016/11/17
Y1 - 2016/11/17
N2 - Multi rotor unmanned aerial vehicle is a hot topic in the field of UAV research. This paper presents a twin rotor copter whose dynamic system is able to tilt. We have a research on the principle of motion and the design of attitude stabilizing controller. Firstly, the dynamics model of the twin rotor aircraft is established. Then the prototype is designed and built to obtain the relevant physical parameters. Finally, the real flight attitude tracking curve was measured by flight experiment which verifies the correctness and effectiveness of the proposed PID attitude controller of the Bi-copter.
AB - Multi rotor unmanned aerial vehicle is a hot topic in the field of UAV research. This paper presents a twin rotor copter whose dynamic system is able to tilt. We have a research on the principle of motion and the design of attitude stabilizing controller. Firstly, the dynamics model of the twin rotor aircraft is established. Then the prototype is designed and built to obtain the relevant physical parameters. Finally, the real flight attitude tracking curve was measured by flight experiment which verifies the correctness and effectiveness of the proposed PID attitude controller of the Bi-copter.
UR - https://www.scopus.com/pages/publications/85006823006
U2 - 10.1109/AUS.2016.7748042
DO - 10.1109/AUS.2016.7748042
M3 - 会议稿件
AN - SCOPUS:85006823006
T3 - AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems
SP - 172
EP - 176
BT - AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016
Y2 - 10 October 2016 through 12 October 2016
ER -