摘要
Dynamic modeling of a hose-drogue aerial refueling system(HDARS)and an integral sliding mode backstepping controller design for the hose whipping phenomenon(HWP)during probe-drogue coupling are studied.Firstly,a dynamic model of the variable-length hose-drogue assembly is built for the sake of exploiting suppression methods for the whipping phenomenon.Based on the lumped parameter method,the hose is modeled by a series of variable-length links connected with frictionless joints.A set of iterative equations of the hose's three-dimensional motion is derived subject to hose reeling in/out,tanker motion,gravity,and aerodynamic loads accounting for the effects of steady wind,atmospheric turbulence,and tanker wake.Secondly,relying on a permanent magnet synchronous motor and high-precision position sensors,a new active control strategy for the HWP on the basis of the relative position between the tanker and the receiver is proposed.Considering the strict-feedback configuration of the permanent magnet synchronous motor,a rotor position control law based on the backstepping method is designed to insure global stability.An integral of the rotor position error and an exponential sliding mode reaching law of the current errors are applied to enhance control accuracy and robustness.Finally,the simulation results show the effectiveness of the proposed model and control laws.
基金
supported by the National Natural Science Foundation of China(No.61304120)
