co-supported by the National Natural Science Foundation of China,China(Nos.51576096 and 51906102);Qing Lan and 333 Project,the Fundamental Research Funds for the Central Universities,China(No.NT2019004);National Science and Technology Major Project China(No.2017-V-0004-0054);Research on the Basic Problem of Intelligent Aero-engine,China(No.2017-JCJQ-ZD-04721);China Postdoctoral Science Foundation Funded Project,China(No.2019M661835);Aeronautics Power Foundation,China(No.6141B09050385)。
In order to compensate for the disturbance of wide variation in rotor demanded torque on power turbine speed and realize the fast response control of turboshaft engine during variable rotor speed,a cascade PID control...
National High-tech Research and Development Program of China(2006AA12A103);National Basic Research Program of China(2010CB731803);Basic Scientific Research Fund of Central Institutions of Higher Education(ZXH2009D006,YWF-10-02-02)
Flight technical error (FTE) combined with navigation system error (NSE) is the main part of total system error (TSE) in performance based navigation (PBN). The implementation of PBN requires pre-flight predic...
Linear quadratic Gaussian with loop transfer recovery (LQG/LTR) gain scheduling technique is utilized to design gain scheduling autopilot for surface-to-air missile. In order to eliminate the artificial uncertaintie...