TY - GEN
T1 - Study on the fault diagnosis method of the five-axis rotor-helicopter
AU - Ding, Yu Hao
AU - Xu, Yong
AU - Zhong, Yuan
N1 - Publisher Copyright:
© 2017 Association for Computing Machinery.
PY - 2017/10/20
Y1 - 2017/10/20
N2 - In this paper, a new model of five-axis rotor helicopter is presented, and the dynamic modeling is carried out. On this basis, for five-axis rotor- helicopter might happen in the motor and blade single fault situation, proportional integral observer was designed and used to on jammed, rotational speed mutation and efficiency decrease fault and diagnosis, which provide the possibility for fault-tolerant control system design.
AB - In this paper, a new model of five-axis rotor helicopter is presented, and the dynamic modeling is carried out. On this basis, for five-axis rotor- helicopter might happen in the motor and blade single fault situation, proportional integral observer was designed and used to on jammed, rotational speed mutation and efficiency decrease fault and diagnosis, which provide the possibility for fault-tolerant control system design.
KW - Dynamic model
KW - Fault diagnosis
KW - Five-axis rotor helicopter
UR - http://www.scopus.com/inward/record.url?scp=85046634994&partnerID=8YFLogxK
U2 - 10.1145/3180496.3180623
DO - 10.1145/3180496.3180623
M3 - Conference contribution
AN - SCOPUS:85046634994
T3 - ACM International Conference Proceeding Series
SP - 151
EP - 155
BT - Proceedings of the 2017 International Conference on Wireless Communications, Networking and Applications, WCNA 2017
A2 - Patnaik, Srikanta
PB - Association for Computing Machinery
T2 - 2017 International Conference on Wireless Communications, Networking and Applications, WCNA 2017
Y2 - 20 October 2017 through 22 October 2017
ER -