شماره 3 تاریخ انتشار 2629-10-23

• Incremental Predictive Command of Velocity to Be Gained Guidance Method
• Gravity-Compensated Robust Control for Micro-Macro Space Manipulators During a Rest to Rest Maneuver
• OPTIMUM DESIGN OF FILAMENT–WOUND LAMINATED CONICAL SHELLS FOR BUCKLING USING THE PENALTY FUNCTION
• Aircraft Visual Identification by Neural Networks
• Vibration analysis of FGM cylindrical shells under various boundary conditions
• VISCOUS NUTATION DAMPER, MODELING AND ANALYSIS