Journal of Aerospace Science and Technology

Journal of Aerospace Science and Technology

Keyword Index
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
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]