Keyword Index

A

  • Aerodynamic loads Plunging Airfoil Load Characteristics Equipped with Gurney Flap [Volume 10, Issue 2, 2013, Pages 25-36]
  • Aircraft Implementation of "MSG-3" for Crack Growth Analysis of Aircraft SSI Components [Volume 10, Issue 1, 2013]
  • Allan Variance Real Time Calibration of Strap-down Three-Axis-Magnetometer for Attitude Estimation [Volume 10, Issue 2, 2013]
  • Analysis Implementation of "MSG-3" for Crack Growth Analysis of Aircraft SSI Components [Volume 10, Issue 1, 2013]
  • Anti-Spoofing A Wavelet-based Spoofing Error Compensation Technique for Single Frequency GPS Stationary Receiver [Volume 10, Issue 2, 2013, Pages 9-16]

B

  • Boundary condition Simulation of Pitching and Heaving Airfoil with Oscillation of Flow Boundary Condition [Volume 10, Issue 1, 2013]

C

  • Central composite design Rotor Sizing of Helicopters Using Statistical Approach [Volume 10, Issue 1, 2013]
  • Central composite design Experimental Investigation ofthe Hovering Performance of aTwin-Rotor Test Model [Volume 10, Issue 2, 2013]
  • Crack Implementation of "MSG-3" for Crack Growth Analysis of Aircraft SSI Components [Volume 10, Issue 1, 2013]

D

  • Dynamic stall Plunging Airfoil Load Characteristics Equipped with Gurney Flap [Volume 10, Issue 2, 2013, Pages 25-36]
  • Dynamic test Nonlinear Dynamic Modeling and Hysteresis Analysis of Aerospace Hydro - dynamical Control Valves [Volume 10, Issue 1, 2013]

F

  • Fuzzy guidance low A Three Stage Terminal Fuzzy Guidance Law for Reentry Vehicles [Volume 10, Issue 1, 2013]

G

  • GPS Spoofing A Wavelet-based Spoofing Error Compensation Technique for Single Frequency GPS Stationary Receiver [Volume 10, Issue 2, 2013, Pages 9-16]
  • Ground effect Optimization of Moving Wingin Ground Effect using Response Surface Method [Volume 10, Issue 2, 2013]
  • Gurney flap Plunging Airfoil Load Characteristics Equipped with Gurney Flap [Volume 10, Issue 2, 2013, Pages 25-36]

H

  • Heaving Simulation of Pitching and Heaving Airfoil with Oscillation of Flow Boundary Condition [Volume 10, Issue 1, 2013]
  • Helicopter Rotor Sizing of Helicopters Using Statistical Approach [Volume 10, Issue 1, 2013]
  • Heuristic Dynamic Programming Extracting Dynamics Matrix of Alignment Process for a Gimbaled Inertial Navigation System Using Heuristic Dynamic Programming Method [Volume 10, Issue 1, 2013]
  • Hoveringperformance Experimental Investigation ofthe Hovering Performance of aTwin-Rotor Test Model [Volume 10, Issue 2, 2013]
  • Hydro - mechanical valve Nonlinear Dynamic Modeling and Hysteresis Analysis of Aerospace Hydro - dynamical Control Valves [Volume 10, Issue 1, 2013]
  • Hysteresis Nonlinear Dynamic Modeling and Hysteresis Analysis of Aerospace Hydro - dynamical Control Valves [Volume 10, Issue 1, 2013]

I

  • Inviscid Simulation of Pitching and Heaving Airfoil with Oscillation of Flow Boundary Condition [Volume 10, Issue 1, 2013]

K

  • Kalman Filter Real Time Calibration of Strap-down Three-Axis-Magnetometer for Attitude Estimation [Volume 10, Issue 2, 2013]

M

  • Magnetometer calibration Real Time Calibration of Strap-down Three-Axis-Magnetometer for Attitude Estimation [Volume 10, Issue 2, 2013]
  • Mathematical Modeling Nonlinear Dynamic Modeling and Hysteresis Analysis of Aerospace Hydro - dynamical Control Valves [Volume 10, Issue 1, 2013]
  • MEMS optical switch Second Order Sliding Mode Observer-Based Control for Uncertain Nonlinear MEMS Optical Switch [Volume 10, Issue 2, 2013]

O

  • Optimal control Extracting Dynamics Matrix of Alignment Process for a Gimbaled Inertial Navigation System Using Heuristic Dynamic Programming Method [Volume 10, Issue 1, 2013]

P

  • Pitchnig Simulation of Pitching and Heaving Airfoil with Oscillation of Flow Boundary Condition [Volume 10, Issue 1, 2013]
  • Plunging airfoil Plunging Airfoil Load Characteristics Equipped with Gurney Flap [Volume 10, Issue 2, 2013, Pages 25-36]

R

  • Reentrym Vehicles A Three Stage Terminal Fuzzy Guidance Law for Reentry Vehicles [Volume 10, Issue 1, 2013]
  • Response Surface Optimization of Moving Wingin Ground Effect using Response Surface Method [Volume 10, Issue 2, 2013]
  • Rotor overlap sweep Experimental Investigation ofthe Hovering Performance of aTwin-Rotor Test Model [Volume 10, Issue 2, 2013]

S

  • Single Frequency Receiver A Wavelet-based Spoofing Error Compensation Technique for Single Frequency GPS Stationary Receiver [Volume 10, Issue 2, 2013, Pages 9-16]
  • SSI Implementation of "MSG-3" for Crack Growth Analysis of Aircraft SSI Components [Volume 10, Issue 1, 2013]
  • Stage terminal A Three Stage Terminal Fuzzy Guidance Law for Reentry Vehicles [Volume 10, Issue 1, 2013]
  • Static condition Optimization of Moving Wingin Ground Effect using Response Surface Method [Volume 10, Issue 2, 2013]
  • StatisticalDesign Rotor Sizing of Helicopters Using Statistical Approach [Volume 10, Issue 1, 2013]
  • Statistic Wavelet Transform A Wavelet-based Spoofing Error Compensation Technique for Single Frequency GPS Stationary Receiver [Volume 10, Issue 2, 2013, Pages 9-16]

T

  • Transoinc Simulation of Pitching and Heaving Airfoil with Oscillation of Flow Boundary Condition [Volume 10, Issue 1, 2013]
  • Twin-rotor Experimental Investigation ofthe Hovering Performance of aTwin-Rotor Test Model [Volume 10, Issue 2, 2013]

U

  • Unscented particle filter Real Time Calibration of Strap-down Three-Axis-Magnetometer for Attitude Estimation [Volume 10, Issue 2, 2013]

V

  • Viscous Simulation of Pitching and Heaving Airfoil with Oscillation of Flow Boundary Condition [Volume 10, Issue 1, 2013]

W

  • Wind tunnel test Experimental Investigation ofthe Hovering Performance of aTwin-Rotor Test Model [Volume 10, Issue 2, 2013]
  • Wing shape Optimization of Moving Wingin Ground Effect using Response Surface Method [Volume 10, Issue 2, 2013]