supported by the State Key Laboratory of Industrial Control Technology Zhejiang University China(No.ICT1447);Shanghai Leading Academic Discipline Project(No.J50103)
Based on a nonlinear flight dynamic model with aerodynamic coefficients and external disturbance uncertainties, which is a typical cyber physical system, a filtering backstepping terminal sliding mode control method i...
supported by the Open Research Project of the State Key Laboratory of Industrial Control Technology Zhejiang University China(No.ICT1401);Shanghai Leading Academic Discipline Project(No.J50103)
A new robust control method of a nonlinear flight dynamic system with aerodynamic coefficients and external disturbance has been proposed.The proposed control system is a combination of the dynamic surface control(DSC...