;Partial Contents: Mathematical Modeling and its Application for Helicopter Maneuver Flight Based on Inverse Simulation; Nonlinear Vibration of Transversely Isotropic Piezoelectric Rectangular Plate; Expert System for Failure Diagnosing and Fatigue Evaluating about Damage of Lugs in Aircraft; A Converter for Switched Reluctance Generator; Hybrid Fuzzy Logic Control by Combining Slide Model and PI for a Nonlinear Flight Control System; Analysis on Dynamic Mold of Spindle of Internal Grinder Based on BP Neural Network.
Journal of Nanjing University of Aeronautics and Astronautics, Volume 35, No. 1, 2003
2003
118 pages
Report
Keine Angabe
Englisch