TY - JOUR
T1 - Feel force control incorporating velocity feedforward and inverse model observer for control loading system of flight simulator
AU - Zhao, Jinsong
AU - Shen, Gang
AU - Yang, Chifu
AU - Liu, Guangda
AU - Yin, Liyi
AU - Han, Junwei
PY - 2013/2
Y1 - 2013/2
N2 - Flight simulator is an essential rig for training pilot, and the control loading system is one of its important components to simulate control force feel of flying in actual airplane. This article states the key factor of control loading system: the disturbance of the flight control displacement on the accuracy of the force loop, that is, the inner loop of control loading system, which affects the fidelity of control force feel simulation. To reduce the disturbance effectively in the inner loop of control loading system, a new strategy, combining velocity feedforward with inverse model observer, is proposed, and the corresponding robust stability analysis is also provided. A transfer function of nonminimum-phase system inverse model, as the inverse model observer, is designed. In order to verify the practical feasibility of the proposed control strategy, experiment is conducted with hardware-in-the-loop- simulation platform based on RT-LAB rapid control prototype. Experimental results demonstrate that the proposed control strategy improves the performance of the control loading system effectively.
AB - Flight simulator is an essential rig for training pilot, and the control loading system is one of its important components to simulate control force feel of flying in actual airplane. This article states the key factor of control loading system: the disturbance of the flight control displacement on the accuracy of the force loop, that is, the inner loop of control loading system, which affects the fidelity of control force feel simulation. To reduce the disturbance effectively in the inner loop of control loading system, a new strategy, combining velocity feedforward with inverse model observer, is proposed, and the corresponding robust stability analysis is also provided. A transfer function of nonminimum-phase system inverse model, as the inverse model observer, is designed. In order to verify the practical feasibility of the proposed control strategy, experiment is conducted with hardware-in-the-loop- simulation platform based on RT-LAB rapid control prototype. Experimental results demonstrate that the proposed control strategy improves the performance of the control loading system effectively.
KW - Control loading system
KW - Electrohydraulic servo control
KW - Flight simulator
KW - Inverse model observer
KW - System identification
UR - http://www.scopus.com/inward/record.url?scp=84877854856&partnerID=8YFLogxK
U2 - 10.1177/0959651812464465
DO - 10.1177/0959651812464465
M3 - 文章
AN - SCOPUS:84877854856
SN - 0959-6518
VL - 227
SP - 161
EP - 175
JO - Proceedings of the Institution of Mechanical Engineers. Part I: Journal of Systems and Control Engineering
JF - Proceedings of the Institution of Mechanical Engineers. Part I: Journal of Systems and Control Engineering
IS - 2
ER -