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journal of aerospace science and technology
سال:2013 - دوره:10 - شماره:1
A Three Stage Terminal Fuzzy Guidance Law for Reentry Vehicles
- صفحه:45-55
Extracting Dynamics Matrix of Alignment Process for a Gimbaled Inertial Navigation System Using Heuristic Dynamic Programming Method
- صفحه:39-43
Implementation of “MSG-3” for Crack Growth Analysis of Aircraft SSI Components
- صفحه:1-15
Nonlinear Dynamic Modeling and Hysteresis Analysis of Aerospace Hydro-dynamical Control Valves
- صفحه:57-68
Rotor Sizing of Helicopters Using Approach Statistical
- صفحه:17-26
Simulation of Pitching and Heaving Airfoil with Oscillation of Flow Boundary Condition
- صفحه:27-37
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