Adaptive attitude controlSatellite Adaptive Attitude Control Based on Decentralized Minimal Control in the Presence of Reaction wheel Accurate Model [Volume 9, Issue 1, 2016, Pages 47-56]
Adaptive attitude controlSatellite Adaptive Attitude Control Based on Decentralized Minimal Control in the Presence of Reaction wheel Accurate Model [Volume 9, Issue 1, 2016, Pages 59-72]
ADCS SimulatorSatellite Spin Stabilization by Magnetic Torquers and Validation with Air-Bearing Simulator [Volume 9, Issue 2, 2016, Pages 25-34]
ADCS SimulatorEvaluation of Magnetic Attitude control with Air-Bearing simulator [Volume 9, Issue 2, 2016, Pages 47-60]
Agility satelliteDesigning and Implemntation of PID and Feed back Quaternion Control Strategies for Three Axis Satellite Simulator Equipped With Control Moment Gyros Actiatprs [Volume 9, Issue 1, 2016, Pages 13-23]
Air bearingSatellite Spin Stabilization by Magnetic Torquers and Validation with Air-Bearing Simulator [Volume 9, Issue 2, 2016, Pages 25-34]
Air bearingEvaluation of Magnetic Attitude control with Air-Bearing simulator [Volume 9, Issue 2, 2016, Pages 47-60]
AngiogenesisThe Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2016, Pages 63-68]
Atmospheric dopplerAtmospheric Doppler Modelling for Open Loop Tracking in GPS-RO Receivers [Volume 9, Issue 2, 2016, Pages 35-46]
Attitude controlDesigning and Implemntation of PID and Feed back Quaternion Control Strategies for Three Axis Satellite Simulator Equipped With Control Moment Gyros Actiatprs [Volume 9, Issue 1, 2016, Pages 13-23]
Attitude controlDesign and Implementation of Backstepping-Sliding mode Attitude Controller in The Prossecor in The Loop Test Bed [Volume 9, Issue 1, 2016, Pages 25-35]
Attitude determinationUsing the Joint Probabilistic Data Association Filter for Improving Star Trackers Performance to Accurate Attitude Determination of Spacecrafts [Volume 9, Issue 1, 2016, Pages 37-46]
Attitude determination(Technical Note)
Design and Construction of Star Tracker Platform in Order to Satellite Attitude Determination Based on Star Tracking Algorithm [Volume 9, Issue 2, 2016, Pages 85-90]
Attitude determination and control subsystemDesign, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]
B
BacksteppingDesign and Implementation of Backstepping-Sliding mode Attitude Controller in The Prossecor in The Loop Test Bed [Volume 9, Issue 1, 2016, Pages 25-35]
Backstepping controlIntegrated Guidance and Control Design by Combining Backstepping and Sliding Mode Control Methods [Volume 9, Issue 4, 2016, Pages 39-50]
Booster turbopumpOptimization of Schematic and Parameters of Staged Combustion Launch Vehicle Liquid Engines [Volume 9, Issue 1, 2016, Pages 1-11]
C
Centroid algorithm(Technical Note)
Design and Construction of Star Tracker Platform in Order to Satellite Attitude Determination Based on Star Tracking Algorithm [Volume 9, Issue 2, 2016, Pages 85-90]
Classical DesignLaunch Vehicle Classical Design Software with Training Approach in Higher Education [Volume 9, Issue 3, 2016, Pages 73-79]
Classical microgravityThe Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2016, Pages 63-68]
Cost ApproachSpace Launch System Family Technology Development Model from Propulsion Aspect with Cost Approach [Volume 9, Issue 4, 2016, Pages 1-12]
D
Data correlationDesign and Manufacture of Thermal Model of AUTSAT Satellite and Its Thermal Balance Test [Volume 9, Issue 2, 2016, Pages 61-76]
Design and constructionDesign, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]
Design optimizationOptimization of Schematic and Parameters of Staged Combustion Launch Vehicle Liquid Engines [Volume 9, Issue 1, 2016, Pages 1-11]
E
Earth observation satelliteDetermine the Optimal Orbit for an Earth Observation Satellite Considering the Power [Volume 9, Issue 3, 2016, Pages 27-36]
Educational ApproachLaunch Vehicle Classical Design Software with Training Approach in Higher Education [Volume 9, Issue 3, 2016, Pages 73-79]
Electrical power subsystemDetermine the Optimal Orbit for an Earth Observation Satellite Considering the Power [Volume 9, Issue 3, 2016, Pages 27-36]
Elliptical earthApproximate Solution of Required Velocity in Elliptical Earth Model Using Piecewise Linear [Volume 9, Issue 3, 2016, Pages 1-12]
Extended jacobeanA Launch Vehicle Tracker Design Based on On-Line Linearization [Volume 9, Issue 2, 2016, Pages 1-9]
Extended kalman Filter (EKF)Reduce Position and Velocity RMS Error of Non-linear Filters in LEO Satellite Radar Tracking [Volume 9, Issue 4, 2016, Pages 51-63]
F
Feed back quaternion strategyDesigning and Implemntation of PID and Feed back Quaternion Control Strategies for Three Axis Satellite Simulator Equipped With Control Moment Gyros Actiatprs [Volume 9, Issue 1, 2016, Pages 13-23]
G
Genetic AlgorithmOptimization of Schematic and Parameters of Staged Combustion Launch Vehicle Liquid Engines [Volume 9, Issue 1, 2016, Pages 1-11]
Geostationary orbitOptimal Trajectory Design of an Upper Stage for Satellite Injection into Geostationary Orbit Using Limited Thrust [Volume 9, Issue 4, 2016, Pages 13-25]
GNSS error predictionOrbit Determination via a Deeply- Coupled UKF/GNSS Filter [Volume 9, Issue 3, 2016, Pages 13-26]
GPS/GNSSOrbit Determination via a Deeply- Coupled UKF/GNSS Filter [Volume 9, Issue 3, 2016, Pages 13-26]
H
Helmholtz coilDesign, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]
Hot-fire testReview of a Swirl Double Base Injector Performance by It’s Hot-Fire Test on a Laboratory Liquid Micro Impulse Engine With Single Injector [Volume 9, Issue 1, 2016, Pages 73-89]
I
IdentificationDesign, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]
ImpulseOptimization of Schematic and Parameters of Staged Combustion Launch Vehicle Liquid Engines [Volume 9, Issue 1, 2016, Pages 1-11]
Integrated guidance and autopilotIntegrated Guidance and Control Design by Combining Backstepping and Sliding Mode Control Methods [Volume 9, Issue 4, 2016, Pages 39-50]
J
JPDAFUsing the Joint Probabilistic Data Association Filter for Improving Star Trackers Performance to Accurate Attitude Determination of Spacecrafts [Volume 9, Issue 1, 2016, Pages 37-46]
L
Launch VehicleLaunch Vehicle Classical Design Software with Training Approach in Higher Education [Volume 9, Issue 3, 2016, Pages 73-79]
Launch vehicle controllerA Launch Vehicle Tracker Design Based on On-Line Linearization [Volume 9, Issue 2, 2016, Pages 1-9]
LEODesign and Manufacture of Thermal Model of AUTSAT Satellite and Its Thermal Balance Test [Volume 9, Issue 2, 2016, Pages 61-76]
LEO satellitesReduce Position and Velocity RMS Error of Non-linear Filters in LEO Satellite Radar Tracking [Volume 9, Issue 4, 2016, Pages 51-63]
Liquid propellant micro engineReview of a Swirl Double Base Injector Performance by It’s Hot-Fire Test on a Laboratory Liquid Micro Impulse Engine With Single Injector [Volume 9, Issue 1, 2016, Pages 73-89]
LVCCD SoftwareLaunch Vehicle Classical Design Software with Training Approach in Higher Education [Volume 9, Issue 3, 2016, Pages 73-79]
M
Magnetic attitude controlEvaluation of Magnetic Attitude control with Air-Bearing simulator [Volume 9, Issue 2, 2016, Pages 47-60]
Magnetic field controllerDesign, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]
Magnetic field simulatorDesign, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]
Magnetic spin controlSatellite Spin Stabilization by Magnetic Torquers and Validation with Air-Bearing Simulator [Volume 9, Issue 2, 2016, Pages 25-34]
MagnetorquerSatellite Spin Stabilization by Magnetic Torquers and Validation with Air-Bearing Simulator [Volume 9, Issue 2, 2016, Pages 25-34]
MagnetorquerEvaluation of Magnetic Attitude control with Air-Bearing simulator [Volume 9, Issue 2, 2016, Pages 47-60]
ModelingDesign, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]
MonitorRole of States in Regulating Space Activities in International Law [Volume 9, Issue 4, 2016, Pages 27-37]
O
On-line linearizationA Launch Vehicle Tracker Design Based on On-Line Linearization [Volume 9, Issue 2, 2016, Pages 1-9]
Open loop trackingAtmospheric Doppler Modelling for Open Loop Tracking in GPS-RO Receivers [Volume 9, Issue 2, 2016, Pages 35-46]
Orbital designDetermine the Optimal Orbit for an Earth Observation Satellite Considering the Power [Volume 9, Issue 3, 2016, Pages 27-36]
Orbit estimationOrbit Determination via a Deeply- Coupled UKF/GNSS Filter [Volume 9, Issue 3, 2016, Pages 13-26]
Outer spaceRole of States in Regulating Space Activities in International Law [Volume 9, Issue 4, 2016, Pages 27-37]
P
Pattern Recognition(Technical Note)
Design and Construction of Star Tracker Platform in Order to Satellite Attitude Determination Based on Star Tracking Algorithm [Volume 9, Issue 2, 2016, Pages 85-90]
PIDDesigning and Implemntation of PID and Feed back Quaternion Control Strategies for Three Axis Satellite Simulator Equipped With Control Moment Gyros Actiatprs [Volume 9, Issue 1, 2016, Pages 13-23]
Piecewise linear gravityApproximate Solution of Required Velocity in Elliptical Earth Model Using Piecewise Linear [Volume 9, Issue 3, 2016, Pages 1-12]
Pin pullerDesign and Fabrication of Spool Type Pin Puller Mechanism- from Concept to Qualification Model [Volume 9, Issue 3, 2016, Pages 37-51]
Pitch programA Launch Vehicle Tracker Design Based on On-Line Linearization [Volume 9, Issue 2, 2016, Pages 1-9]
Pole placement theoryA Launch Vehicle Tracker Design Based on On-Line Linearization [Volume 9, Issue 2, 2016, Pages 1-9]
Propulsion SystemSpace Launch System Family Technology Development Model from Propulsion Aspect with Cost Approach [Volume 9, Issue 4, 2016, Pages 1-12]
Pyramid algorithmUsing the Joint Probabilistic Data Association Filter for Improving Star Trackers Performance to Accurate Attitude Determination of Spacecrafts [Volume 9, Issue 1, 2016, Pages 37-46]
R
Radar observationReduce Position and Velocity RMS Error of Non-linear Filters in LEO Satellite Radar Tracking [Volume 9, Issue 4, 2016, Pages 51-63]
Radio occultationAtmospheric Doppler Modelling for Open Loop Tracking in GPS-RO Receivers [Volume 9, Issue 2, 2016, Pages 35-46]
RatThe Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2016, Pages 63-68]
Reaction wheelDesign and Implementation of Backstepping-Sliding mode Attitude Controller in The Prossecor in The Loop Test Bed [Volume 9, Issue 1, 2016, Pages 25-35]
Reaction wheel modelSatellite Adaptive Attitude Control Based on Decentralized Minimal Control in the Presence of Reaction wheel Accurate Model [Volume 9, Issue 1, 2016, Pages 47-56]
Reaction wheel modelSatellite Adaptive Attitude Control Based on Decentralized Minimal Control in the Presence of Reaction wheel Accurate Model [Volume 9, Issue 1, 2016, Pages 59-72]
Relaxation mechanismsDesign and Fabrication of Spool Type Pin Puller Mechanism- from Concept to Qualification Model [Volume 9, Issue 3, 2016, Pages 37-51]
Repeating ground trackDetermining orbital element on Earth Observation Repeat-Ground-Track orbit [Volume 9, Issue 2, 2016, Pages 77-83]
Required velocityApproximate Solution of Required Velocity in Elliptical Earth Model Using Piecewise Linear [Volume 9, Issue 3, 2016, Pages 1-12]
ResponsibilityRole of States in Regulating Space Activities in International Law [Volume 9, Issue 4, 2016, Pages 27-37]
S
Satellite’s magnetic testsDesign, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]
Semi-cryogenicSpace Launch System Family Technology Development Model from Propulsion Aspect with Cost Approach [Volume 9, Issue 4, 2016, Pages 1-12]
SimulationDetermine the Optimal Orbit for an Earth Observation Satellite Considering the Power [Volume 9, Issue 3, 2016, Pages 27-36]
Simulator of satelliteDesigning and Implemntation of PID and Feed back Quaternion Control Strategies for Three Axis Satellite Simulator Equipped With Control Moment Gyros Actiatprs [Volume 9, Issue 1, 2016, Pages 13-23]
Single gimbal control moment gyroscopeDesigning and Implemntation of PID and Feed back Quaternion Control Strategies for Three Axis Satellite Simulator Equipped With Control Moment Gyros Actiatprs [Volume 9, Issue 1, 2016, Pages 13-23]
Sliding modeDesign and Implementation of Backstepping-Sliding mode Attitude Controller in The Prossecor in The Loop Test Bed [Volume 9, Issue 1, 2016, Pages 25-35]
Sliding mode controlIntegrated Guidance and Control Design by Combining Backstepping and Sliding Mode Control Methods [Volume 9, Issue 4, 2016, Pages 39-50]
Small satelliteDesign and Manufacture of Thermal Model of AUTSAT Satellite and Its Thermal Balance Test [Volume 9, Issue 2, 2016, Pages 61-76]
Software in the loopDesign and Implementation of Backstepping-Sliding mode Attitude Controller in The Prossecor in The Loop Test Bed [Volume 9, Issue 1, 2016, Pages 25-35]
SovereigntyRole of States in Regulating Space Activities in International Law [Volume 9, Issue 4, 2016, Pages 27-37]
Space activitiesRole of States in Regulating Space Activities in International Law [Volume 9, Issue 4, 2016, Pages 27-37]
Space boomIdentification of Space Deployable Mechanisms [Volume 9, Issue 3, 2016, Pages 53-71]
Space deployable mechanismIdentification of Space Deployable Mechanisms [Volume 9, Issue 3, 2016, Pages 53-71]
Space Inflatable devicesIdentification of Space Deployable Mechanisms [Volume 9, Issue 3, 2016, Pages 53-71]
Staged combustionOptimization of Schematic and Parameters of Staged Combustion Launch Vehicle Liquid Engines [Volume 9, Issue 1, 2016, Pages 1-11]
Star catalog(Technical Note)
Design and Construction of Star Tracker Platform in Order to Satellite Attitude Determination Based on Star Tracking Algorithm [Volume 9, Issue 2, 2016, Pages 85-90]
Star neighborhood approachUsing the Joint Probabilistic Data Association Filter for Improving Star Trackers Performance to Accurate Attitude Determination of Spacecrafts [Volume 9, Issue 1, 2016, Pages 37-46]
Star trackerUsing the Joint Probabilistic Data Association Filter for Improving Star Trackers Performance to Accurate Attitude Determination of Spacecrafts [Volume 9, Issue 1, 2016, Pages 37-46]
Star tracker(Technical Note)
Design and Construction of Star Tracker Platform in Order to Satellite Attitude Determination Based on Star Tracking Algorithm [Volume 9, Issue 2, 2016, Pages 85-90]
Steering lawDesigning and Implemntation of PID and Feed back Quaternion Control Strategies for Three Axis Satellite Simulator Equipped With Control Moment Gyros Actiatprs [Volume 9, Issue 1, 2016, Pages 13-23]
STK softwareReduce Position and Velocity RMS Error of Non-linear Filters in LEO Satellite Radar Tracking [Volume 9, Issue 4, 2016, Pages 51-63]
Swirl injectorReview of a Swirl Double Base Injector Performance by It’s Hot-Fire Test on a Laboratory Liquid Micro Impulse Engine With Single Injector [Volume 9, Issue 1, 2016, Pages 73-89]
T
Technology DevelopmentSpace Launch System Family Technology Development Model from Propulsion Aspect with Cost Approach [Volume 9, Issue 4, 2016, Pages 1-12]
Thermal balance testDesign and Manufacture of Thermal Model of AUTSAT Satellite and Its Thermal Balance Test [Volume 9, Issue 2, 2016, Pages 61-76]
Thermal modelDesign and Manufacture of Thermal Model of AUTSAT Satellite and Its Thermal Balance Test [Volume 9, Issue 2, 2016, Pages 61-76]
Thermodynamic cycleOptimization of Schematic and Parameters of Staged Combustion Launch Vehicle Liquid Engines [Volume 9, Issue 1, 2016, Pages 1-11]
ThrustReview of a Swirl Double Base Injector Performance by It’s Hot-Fire Test on a Laboratory Liquid Micro Impulse Engine With Single Injector [Volume 9, Issue 1, 2016, Pages 73-89]
Ttwo point homing interceptionIntegrated Guidance and Control Design by Combining Backstepping and Sliding Mode Control Methods [Volume 9, Issue 4, 2016, Pages 39-50]
U
Uncertainty and actuator saturationSatellite Adaptive Attitude Control Based on Decentralized Minimal Control in the Presence of Reaction wheel Accurate Model [Volume 9, Issue 1, 2016, Pages 47-56]
Uncertainty and actuator saturationSatellite Adaptive Attitude Control Based on Decentralized Minimal Control in the Presence of Reaction wheel Accurate Model [Volume 9, Issue 1, 2016, Pages 59-72]
Unscented kalman Filter (UKF)Orbit Determination via a Deeply- Coupled UKF/GNSS Filter [Volume 9, Issue 3, 2016, Pages 13-26]
Unscented kalman Filter (UKF)Reduce Position and Velocity RMS Error of Non-linear Filters in LEO Satellite Radar Tracking [Volume 9, Issue 4, 2016, Pages 51-63]
V
Vacuum temperature testsDesign and Fabrication of Spool Type Pin Puller Mechanism- from Concept to Qualification Model [Volume 9, Issue 3, 2016, Pages 37-51]
VEGFThe Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2016, Pages 63-68]
Vibration testsDesign and Fabrication of Spool Type Pin Puller Mechanism- from Concept to Qualification Model [Volume 9, Issue 3, 2016, Pages 37-51]