TY - JOUR
T1 - Coordinated Turn of Fixed-Wing Aircraft under Wind Interface on Integral Backstepping
AU - Song, Yuecheng
AU - Liu, Zhenbao
AU - Han, Junwei
AU - Zhao, Wen
AU - Li, Ni
N1 - Publisher Copyright:
© 1963-2012 IEEE.
PY - 2021
Y1 - 2021
N2 - In windy environments, coordinated turning stabilization and high precise of positioning are very vulnerable, and many studies have made it the main goal in their studies. In this article, a new control strategy of stabilizing the fixed-wing aircraft has been introduced in windy environments. First of all, in order to keep the aircraft itself stable, a new type of sliding mode control strategy is applied for control of the attitude and position. Second, we analyze the proposed model in windy environments based on the designed control strategy. Third but the most important, a radial basis function (RBF) network is introduced for decreasing the disturbance error and minimizing the effect of the disturbance. The airplane model has been simulated on many wind conditions in different flying status. We have also applied our control theory to the real flying experiments. From the experiments, it can be clearly found that the proposed method works well in a large range of windy environments and flying status, proposing that our method is effective in the winds.
AB - In windy environments, coordinated turning stabilization and high precise of positioning are very vulnerable, and many studies have made it the main goal in their studies. In this article, a new control strategy of stabilizing the fixed-wing aircraft has been introduced in windy environments. First of all, in order to keep the aircraft itself stable, a new type of sliding mode control strategy is applied for control of the attitude and position. Second, we analyze the proposed model in windy environments based on the designed control strategy. Third but the most important, a radial basis function (RBF) network is introduced for decreasing the disturbance error and minimizing the effect of the disturbance. The airplane model has been simulated on many wind conditions in different flying status. We have also applied our control theory to the real flying experiments. From the experiments, it can be clearly found that the proposed method works well in a large range of windy environments and flying status, proposing that our method is effective in the winds.
KW - Coordinate turning
KW - fixed-wing aircraft
KW - integral sliding mode
KW - radial basis function (RBF) network
KW - wind turbulence
UR - http://www.scopus.com/inward/record.url?scp=85118543672&partnerID=8YFLogxK
U2 - 10.1109/TIM.2021.3122169
DO - 10.1109/TIM.2021.3122169
M3 - 文章
AN - SCOPUS:85118543672
SN - 0018-9456
VL - 70
JO - IEEE Transactions on Instrumentation and Measurement
JF - IEEE Transactions on Instrumentation and Measurement
ER -