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journal of aerospace science and technology
سال:2012 - دوره:9 - شماره:2
A Novel System-Level Calibration Method for Gimballed Platform IMU Using Optimal Estimation
- صفحه:1-13
An Experimental Investigation of the Effects of Canard Position on the Aerodynamic Forces ofaFighter Type Configuration Model
- صفحه:15-23
Approximate Solution of Sensitivity Matrix of Required Velocity Using Piecewise Linear Gravity Assumption
- صفحه:25-31
Intelligent Auto pilot Design for a Nonlinear Model of an Autonomous Helicopter by Adaptive Emotional Approach
- صفحه:33-43
Novel Radial Basis Function Neural Networks based on Probabilistic Evolutionary and Gaussian Mixture Model for Satellites Optimum Selection
- صفحه:71-81
Parametric Study of the Empty and Foam-Filled End-Capped Conical Tubes under Quasi Static and Dynamic Impact Loads
- صفحه:59-70
The Utilization of High Fidelity Simulation in the Support of UAV Launch Phase Design: Three Case Studies
- صفحه:45-57
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