Journal of Aerospace Science and Technology

Journal of Aerospace Science and Technology

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]