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journal of aerospace science and technology
سال:2017 - دوره:11 - شماره:1
Active Vibration Suppression of a Nonlinear Flexible Spacecraft
- صفحه:35-46
Airfoil Shape Optimization with Adaptive Mutation Genetic Algorithm
- صفحه:47-59
Loading Estimation of Flapping Wings under Aeroelastic Effect Using Finite Element Method
- صفحه:9-20
Local Imperfection Effects on Thermal Buckling Behavior of Composite Fiber Reinforced Truncated Conical Liner
- صفحه:21-34
Preliminary Design of Spacecraft Attitude Control with Pulse-Width Pulse-Frequency Modulator for Rest-to-Rest Maneuvers
- صفحه:1-8
Robust Fixed-order Gain-scheduling Autopilot Design using State-space Stability-Preserving Interpolation
- صفحه:61-73
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