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]