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]