Accident Investigation MethodsInvestigation of Current Military Aircraft Accidents Investigation Model and Presenting a New Model, Considering the Newly Suggested Accidents Investigation Methods [Volume 17, Issue 1, 2015, Pages 35-52]
Aircraft IndustryIdentifying the Challenges of Innovation and Providing Solutions in Aircraft Industry by the Comparative Study of South Korea [Volume 17, Issue 2, 2015, Pages 10-22]
Allan VarianceExperimental Calibration and Error Identification of Micro Electro-Mechanical Systems [Volume 17, Issue 1, 2015, Pages 1-9]
Augmented proportional navigationParametric Optimization of Augmented Proportional Navigation Law Considering Performance and Maneuvering Capabilities [Volume 17, Issue 1, 2015, Pages 65-74]
B
BroachingThe effect of rake angle and cutting speed on residual stress in broaching process of Ti6Al4V for air engines [Volume 17, Issue 2, 2015, Pages 73-81]
Challenge of InnovationIdentifying the Challenges of Innovation and Providing Solutions in Aircraft Industry by the Comparative Study of South Korea [Volume 17, Issue 2, 2015, Pages 10-22]
Continues Descent Approach (CDA)Improving Safety in the TABRIZ Airport via Precision Approach Based on Continues Descent [Volume 17, Issue 2, 2015, Pages 82-89]
CrashworthinessThe energy absorption characteristics of tapered honeycomb sandwich cylindrical columns under axial crushing loads [Volume 17, Issue 2, 2015, Pages 1-9]
Cutting SpeedThe effect of rake angle and cutting speed on residual stress in broaching process of Ti6Al4V for air engines [Volume 17, Issue 2, 2015, Pages 73-81]
D
Dynamic ModelOffering the model based on system dynamics for improvement of flight safety [Volume 17, Issue 2, 2015, Pages 44-56]
E
EmergencyFlight Management System design for Emergency Conditions [Volume 17, Issue 1, 2015, Pages 53-64]
Emergency LandingMulti-Objective Emergency Landing Trajectory Design Based on Motion Primitives [Volume 17, Issue 2, 2015, Pages 57-72]
Energy absorptionThe energy absorption characteristics of tapered honeycomb sandwich cylindrical columns under axial crushing loads [Volume 17, Issue 2, 2015, Pages 1-9]
F
Failure analysisThe effect of design parameters on light aircraft flaps mechanism’s reliability [Volume 17, Issue 1, 2015, Pages 75-82]
Fault Tree AnalysisThe effect of design parameters on light aircraft flaps mechanism’s reliability [Volume 17, Issue 1, 2015, Pages 75-82]
Flap mechanismThe effect of design parameters on light aircraft flaps mechanism’s reliability [Volume 17, Issue 1, 2015, Pages 75-82]
Flight management systemFlight Management System design for Emergency Conditions [Volume 17, Issue 1, 2015, Pages 53-64]
Flight safetyOffering the model based on system dynamics for improvement of flight safety [Volume 17, Issue 2, 2015, Pages 44-56]
G
Genetic AlgorithmOptimal combination of inertial sensors for initial alignment of strapdown navigation system using genetic algorithm [Volume 17, Issue 1, 2015, Pages 22-34]
I
Inertial NavigationOptimal combination of inertial sensors for initial alignment of strapdown navigation system using genetic algorithm [Volume 17, Issue 1, 2015, Pages 22-34]
Initial alignmentOptimal combination of inertial sensors for initial alignment of strapdown navigation system using genetic algorithm [Volume 17, Issue 1, 2015, Pages 22-34]
Integrated guidance and controlParametric Optimization of Augmented Proportional Navigation Law Considering Performance and Maneuvering Capabilities [Volume 17, Issue 1, 2015, Pages 65-74]
L
Lambda Shaped WingExperimental Investigation of The Flow Field Over a Non-Slender lambda Shaped Wing by Pressure Measurement [Volume 17, Issue 1, 2015, Pages 10-21]
Light aircraftThe effect of design parameters on light aircraft flaps mechanism’s reliability [Volume 17, Issue 1, 2015, Pages 75-82]
M
Micro Electro-Mechanical systemsExperimental Calibration and Error Identification of Micro Electro-Mechanical Systems [Volume 17, Issue 1, 2015, Pages 1-9]
Military AircraftInvestigation of Current Military Aircraft Accidents Investigation Model and Presenting a New Model, Considering the Newly Suggested Accidents Investigation Methods [Volume 17, Issue 1, 2015, Pages 35-52]
Model of Aircraft Accidents InvestigationInvestigation of Current Military Aircraft Accidents Investigation Model and Presenting a New Model, Considering the Newly Suggested Accidents Investigation Methods [Volume 17, Issue 1, 2015, Pages 35-52]
Motion PrimitivesMulti-Objective Emergency Landing Trajectory Design Based on Motion Primitives [Volume 17, Issue 2, 2015, Pages 57-72]
Multi-Objective OptimizationParametric Optimization of Augmented Proportional Navigation Law Considering Performance and Maneuvering Capabilities [Volume 17, Issue 1, 2015, Pages 65-74]
P
Penetration in soil and concreteتحلیل عددی نفوذ بمبهای سنگرشکن با انرژی جنبشی غیرهستهای (GBU) در سازههای زیرزمینی [Volume 17, Issue 2, 2015, Pages 23-43]
Performance constraintsParametric Optimization of Augmented Proportional Navigation Law Considering Performance and Maneuvering Capabilities [Volume 17, Issue 1, 2015, Pages 65-74]
Pitot TubesExperimental Investigation of The Flow Field Over a Non-Slender lambda Shaped Wing by Pressure Measurement [Volume 17, Issue 1, 2015, Pages 10-21]
Precision ApproachImproving Safety in the TABRIZ Airport via Precision Approach Based on Continues Descent [Volume 17, Issue 2, 2015, Pages 82-89]
Preflight checksThe effect of design parameters on light aircraft flaps mechanism’s reliability [Volume 17, Issue 1, 2015, Pages 75-82]
Pressure distributionExperimental Investigation of The Flow Field Over a Non-Slender lambda Shaped Wing by Pressure Measurement [Volume 17, Issue 1, 2015, Pages 10-21]
R
Residual stressesThe effect of rake angle and cutting speed on residual stress in broaching process of Ti6Al4V for air engines [Volume 17, Issue 2, 2015, Pages 73-81]
S
Safe landingFlight Management System design for Emergency Conditions [Volume 17, Issue 1, 2015, Pages 53-64]
T
TABRIZ airportImproving Safety in the TABRIZ Airport via Precision Approach Based on Continues Descent [Volume 17, Issue 2, 2015, Pages 82-89]
Trajectory PlanningMulti-Objective Emergency Landing Trajectory Design Based on Motion Primitives [Volume 17, Issue 2, 2015, Pages 57-72]
Transformation MatrixOptimal combination of inertial sensors for initial alignment of strapdown navigation system using genetic algorithm [Volume 17, Issue 1, 2015, Pages 22-34]
Weighted least squaresExperimental Calibration and Error Identification of Micro Electro-Mechanical Systems [Volume 17, Issue 1, 2015, Pages 1-9]
Wind tunnelExperimental Investigation of The Flow Field Over a Non-Slender lambda Shaped Wing by Pressure Measurement [Volume 17, Issue 1, 2015, Pages 10-21]
