شماره 1 تاریخ انتشار 2638-04-21

• Loading Estimation of Flapping Wings under Aeroelastic Effect Using Finite Element Method
• Active Vibration Suppression of a Nonlinear Flexible Spacecraft
• Airfoil Shape Optimization with Adaptive Mutation Genetic Algorithm
• Robust Fixed-order Gain-scheduling Autopilot Design using State-space Stability-Preserving Interpolation
• Preliminary Design of Spacecraft Attitude Control with Pulse-Width Pulse-Frequency Modulator for Rest-to-Rest Maneuvers
• Local Imperfection Effects on Thermal Buckling Behavior of Composite Fiber Reinforced Truncated Conical Liner