B
-
BELBIC
Intelligent Auto pilot Design for a Nonlinear Model of an Autonomous Helicopter by Adaptive Emotional Approach [Volume 9, Issue 2, 2012]
C
-
Canard Position
An Experimental Investigation of the Effects of Canard Position on the Aerodynamic Forces of a Fighter Type Configuration Model [Volume 9, Issue 2, 2012, Pages 15-24]
-
CFD
Helicopter Rotor Airloads Prediction Using CFD and Flight Test Measurement in Hover Flight [Volume 9, Issue 1, 2012]
D
-
Dynamic Impact
Parametric Study of the Empty and Foam-Filled End-Capped Conical Tubes under quasi Static and Dynamic impact Loads [Volume 9, Issue 2, 2012]
-
Dynamic mesh
Helicopter Rotor Airloads Prediction Using CFD and Flight Test Measurement in Hover Flight [Volume 9, Issue 1, 2012]
-
Dynamic Model
Practical Evaluation of EKF1 and UKF2 Filters for Terrain Aided Navigation [Volume 9, Issue 1, 2012]
E
-
EKF
A Novel System-Level Calibration Method for Gimballed Platform IMU Using Optimal Estimation [Volume 9, Issue 2, 2012]
-
End-Capped Conical Tubes
Parametric Study of the Empty and Foam-Filled End-Capped Conical Tubes under quasi Static and Dynamic impact Loads [Volume 9, Issue 2, 2012]
-
Extended Kalman Filter
Practical Evaluation of EKF1 and UKF2 Filters for Terrain Aided Navigation [Volume 9, Issue 1, 2012]
F
-
FE-EFG Method
Crack Analysis, Using a New Coupled FE-EFG Method [Volume 9, Issue 1, 2012]
-
Fighter Model
An Experimental Investigation of the Effects of Canard Position on the Aerodynamic Forces of a Fighter Type Configuration Model [Volume 9, Issue 2, 2012, Pages 15-24]
-
Flight Test
Helicopter Rotor Airloads Prediction Using CFD and Flight Test Measurement in Hover Flight [Volume 9, Issue 1, 2012]
-
Fuzzy
A Comprehensive Approach to Develop a Continuous Fuzzy Guidance Law for Maneuvering Targets [Volume 9, Issue 1, 2012]
G
-
Gaussian Mixture
Novel Radial Basis Function Neural Networks based on Probabilistic Evolutionary and Gaussian Mixture Model for Satellites Optimum Selection [Volume 9, Issue 2, 2012]
-
Gimballed IMU
A Novel System-Level Calibration Method for Gimballed Platform IMU Using Optimal Estimation [Volume 9, Issue 2, 2012]
I
-
Inertial Navigation System
Practical Evaluation of EKF1 and UKF2 Filters for Terrain Aided Navigation [Volume 9, Issue 1, 2012]
M
-
Maneuver
A Comprehensive Approach to Develop a Continuous Fuzzy Guidance Law for Maneuvering Targets [Volume 9, Issue 1, 2012]
-
Model Helicopter
Intelligent Auto pilot Design for a Nonlinear Model of an Autonomous Helicopter by Adaptive Emotional Approach [Volume 9, Issue 2, 2012]
-
Moving Reference Frame
Helicopter Rotor Airloads Prediction Using CFD and Flight Test Measurement in Hover Flight [Volume 9, Issue 1, 2012]
N
-
Neural Networks
Novel Radial Basis Function Neural Networks based on Probabilistic Evolutionary and Gaussian Mixture Model for Satellites Optimum Selection [Volume 9, Issue 2, 2012]
-
Nonlinear Model
Intelligent Auto pilot Design for a Nonlinear Model of an Autonomous Helicopter by Adaptive Emotional Approach [Volume 9, Issue 2, 2012]
P
-
PID Controller
Intelligent Auto pilot Design for a Nonlinear Model of an Autonomous Helicopter by Adaptive Emotional Approach [Volume 9, Issue 2, 2012]
-
Probabilistic Evolutionary
Novel Radial Basis Function Neural Networks based on Probabilistic Evolutionary and Gaussian Mixture Model for Satellites Optimum Selection [Volume 9, Issue 2, 2012]
S
-
Satellites Selection
Novel Radial Basis Function Neural Networks based on Probabilistic Evolutionary and Gaussian Mixture Model for Satellites Optimum Selection [Volume 9, Issue 2, 2012]
T
-
Turbulence model
An Innovation in Film Cooling of the Gas Turbine Blades Applying an Upstream Jet [Volume 9, Issue 1, 2012]
U
-
Unscented Kalman filter
Practical Evaluation of EKF1 and UKF2 Filters for Terrain Aided Navigation [Volume 9, Issue 1, 2012]
V
-
Vortex
Effect of Wing Sweep Angle on the Vortex Interaction of a Tail-Wing Configuration [Volume 9, Issue 1, 2012]
W
-
Wind tunnel
Effect of Wing Sweep Angle on the Vortex Interaction of a Tail-Wing Configuration [Volume 9, Issue 1, 2012]
-
Wind tunnel
An Experimental Investigation of the Effects of Canard Position on the Aerodynamic Forces of a Fighter Type Configuration Model [Volume 9, Issue 2, 2012, Pages 15-24]