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journal of aerospace science and technology
سال:2011 - دوره:8 - شماره:2
A Bayesian Networks Approach to Reliability Analysis of a Launch Vehicle Liquid Propellant Engine
- صفحه:107-117
A Control Method Based on the Dynamic Response of the Airplane for Compensation of Pilot-Induced Oscillations: Benefits and Flaws
- صفحه:119-125
An Experimental Study of a Compound Control Method around a Cylinder
- صفحه:97-105
Flow Field Characteristics of an Aerospike Nozzle, Using Different Turbulence Models
- صفحه:127-133
Midcourse Trajectory Shaping for Air and Ballistic Defence Guidance, Using Bezier Curves
- صفحه:87-95
Nonlinear Guidance Law with Finite-Time Convergence Considering Control Loop Dynamics
- صفحه:69-75
Process Improvement of Experimental Measurements, Using D-optimal Models
- صفحه:77-86
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