A
-
Adaptive attitude control
Satellite 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 control
Satellite 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 Simulator
Satellite Spin Stabilization by Magnetic Torquers and Validation with Air-Bearing Simulator [Volume 9, Issue 2, 2016, Pages 25-34]
-
ADCS Simulator
Evaluation of Magnetic Attitude control with Air-Bearing simulator [Volume 9, Issue 2, 2016, Pages 47-60]
-
Agility satellite
Designing 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 bearing
Satellite Spin Stabilization by Magnetic Torquers and Validation with Air-Bearing Simulator [Volume 9, Issue 2, 2016, Pages 25-34]
-
Air bearing
Evaluation of Magnetic Attitude control with Air-Bearing simulator [Volume 9, Issue 2, 2016, Pages 47-60]
-
Angiogenesis
The Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2016, Pages 63-68]
-
Atmospheric doppler
Atmospheric Doppler Modelling for Open Loop Tracking in GPS-RO Receivers [Volume 9, Issue 2, 2016, Pages 35-46]
-
Attitude control
Designing 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 control
Design 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 determination
Using 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 subsystem
Design, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]
B
-
Backstepping
Design 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 control
Integrated Guidance and Control Design by Combining Backstepping and Sliding Mode Control Methods [Volume 9, Issue 4, 2016, Pages 39-50]
-
Booster turbopump
Optimization 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 Design
Launch Vehicle Classical Design Software with Training Approach in Higher Education [Volume 9, Issue 3, 2016, Pages 73-79]
-
Classical microgravity
The Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2016, Pages 63-68]
-
Cost Approach
Space Launch System Family Technology Development Model from Propulsion Aspect with Cost Approach [Volume 9, Issue 4, 2016, Pages 1-12]
D
-
Data correlation
Design and Manufacture of Thermal Model of AUTSAT Satellite and Its Thermal Balance Test [Volume 9, Issue 2, 2016, Pages 61-76]
-
Design and construction
Design, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]
-
Design optimization
Optimization of Schematic and Parameters of Staged Combustion Launch Vehicle Liquid Engines [Volume 9, Issue 1, 2016, Pages 1-11]
E
-
Earth observation satellite
Determine the Optimal Orbit for an Earth Observation Satellite Considering the Power [Volume 9, Issue 3, 2016, Pages 27-36]
-
Educational Approach
Launch Vehicle Classical Design Software with Training Approach in Higher Education [Volume 9, Issue 3, 2016, Pages 73-79]
-
Electrical power subsystem
Determine the Optimal Orbit for an Earth Observation Satellite Considering the Power [Volume 9, Issue 3, 2016, Pages 27-36]
-
Elliptical earth
Approximate Solution of Required Velocity in Elliptical Earth Model Using Piecewise Linear [Volume 9, Issue 3, 2016, Pages 1-12]
-
Extended jacobean
A 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 strategy
Designing 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 algorithm
Optimization of Schematic and Parameters of Staged Combustion Launch Vehicle Liquid Engines [Volume 9, Issue 1, 2016, Pages 1-11]
-
Geostationary orbit
Optimal 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 prediction
Orbit Determination via a Deeply- Coupled UKF/GNSS Filter [Volume 9, Issue 3, 2016, Pages 13-26]
-
GPS/GNSS
Orbit Determination via a Deeply- Coupled UKF/GNSS Filter [Volume 9, Issue 3, 2016, Pages 13-26]
H
-
Helmholtz coil
Design, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]
-
Hot-fire test
Review 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
-
Identification
Design, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]
-
Impulse
Optimization of Schematic and Parameters of Staged Combustion Launch Vehicle Liquid Engines [Volume 9, Issue 1, 2016, Pages 1-11]
-
Integrated guidance and autopilot
Integrated Guidance and Control Design by Combining Backstepping and Sliding Mode Control Methods [Volume 9, Issue 4, 2016, Pages 39-50]
J
-
JPDAF
Using 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 Vehicle
Launch Vehicle Classical Design Software with Training Approach in Higher Education [Volume 9, Issue 3, 2016, Pages 73-79]
-
Launch vehicle controller
A Launch Vehicle Tracker Design Based on On-Line Linearization [Volume 9, Issue 2, 2016, Pages 1-9]
-
LEO
Design and Manufacture of Thermal Model of AUTSAT Satellite and Its Thermal Balance Test [Volume 9, Issue 2, 2016, Pages 61-76]
-
LEO satellites
Reduce 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 engine
Review 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 Software
Launch Vehicle Classical Design Software with Training Approach in Higher Education [Volume 9, Issue 3, 2016, Pages 73-79]
M
-
Magnetic attitude control
Evaluation of Magnetic Attitude control with Air-Bearing simulator [Volume 9, Issue 2, 2016, Pages 47-60]
-
Magnetic field controller
Design, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]
-
Magnetic field simulator
Design, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]
-
Magnetic spin control
Satellite Spin Stabilization by Magnetic Torquers and Validation with Air-Bearing Simulator [Volume 9, Issue 2, 2016, Pages 25-34]
-
Magnetorquer
Satellite Spin Stabilization by Magnetic Torquers and Validation with Air-Bearing Simulator [Volume 9, Issue 2, 2016, Pages 25-34]
-
Magnetorquer
Evaluation of Magnetic Attitude control with Air-Bearing simulator [Volume 9, Issue 2, 2016, Pages 47-60]
-
Modeling
Design, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]
-
Monitor
Role of States in Regulating Space Activities in International Law [Volume 9, Issue 4, 2016, Pages 27-37]
O
-
On-line linearization
A Launch Vehicle Tracker Design Based on On-Line Linearization [Volume 9, Issue 2, 2016, Pages 1-9]
-
Open loop tracking
Atmospheric Doppler Modelling for Open Loop Tracking in GPS-RO Receivers [Volume 9, Issue 2, 2016, Pages 35-46]
-
Orbital design
Determine the Optimal Orbit for an Earth Observation Satellite Considering the Power [Volume 9, Issue 3, 2016, Pages 27-36]
-
Orbital mechanics-satellite orbit design
Determining orbital element on Earth Observation Repeat-Ground-Track orbit [Volume 9, Issue 2, 2016, Pages 77-83]
-
Orbit estimation
Orbit Determination via a Deeply- Coupled UKF/GNSS Filter [Volume 9, Issue 3, 2016, Pages 13-26]
-
Outer space
Role 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]
-
PID
Designing 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 gravity
Approximate Solution of Required Velocity in Elliptical Earth Model Using Piecewise Linear [Volume 9, Issue 3, 2016, Pages 1-12]
-
Pin puller
Design and Fabrication of Spool Type Pin Puller Mechanism- from Concept to Qualification Model [Volume 9, Issue 3, 2016, Pages 37-51]
-
Pitch program
A Launch Vehicle Tracker Design Based on On-Line Linearization [Volume 9, Issue 2, 2016, Pages 1-9]
-
Pole placement theory
A Launch Vehicle Tracker Design Based on On-Line Linearization [Volume 9, Issue 2, 2016, Pages 1-9]
-
Propulsion System
Space Launch System Family Technology Development Model from Propulsion Aspect with Cost Approach [Volume 9, Issue 4, 2016, Pages 1-12]
-
Pyramid algorithm
Using 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 observation
Reduce Position and Velocity RMS Error of Non-linear Filters in LEO Satellite Radar Tracking [Volume 9, Issue 4, 2016, Pages 51-63]
-
Radio occultation
Atmospheric Doppler Modelling for Open Loop Tracking in GPS-RO Receivers [Volume 9, Issue 2, 2016, Pages 35-46]
-
Rat
The Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2016, Pages 63-68]
-
Reaction wheel
Design 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 model
Satellite 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 model
Satellite 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 mechanisms
Design and Fabrication of Spool Type Pin Puller Mechanism- from Concept to Qualification Model [Volume 9, Issue 3, 2016, Pages 37-51]
-
Repeating ground track
Determining orbital element on Earth Observation Repeat-Ground-Track orbit [Volume 9, Issue 2, 2016, Pages 77-83]
-
Required velocity
Approximate Solution of Required Velocity in Elliptical Earth Model Using Piecewise Linear [Volume 9, Issue 3, 2016, Pages 1-12]
-
Responsibility
Role of States in Regulating Space Activities in International Law [Volume 9, Issue 4, 2016, Pages 27-37]
S
-
Satellite’s magnetic tests
Design, Construction, Test and Modeling of Triaxial Helmholtz Coil for Magnetic Tests of Satellite [Volume 9, Issue 2, 2016, Pages 11-24]
-
Semi-cryogenic
Space Launch System Family Technology Development Model from Propulsion Aspect with Cost Approach [Volume 9, Issue 4, 2016, Pages 1-12]
-
Simulation
Determine the Optimal Orbit for an Earth Observation Satellite Considering the Power [Volume 9, Issue 3, 2016, Pages 27-36]
-
Simulator of satellite
Designing 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 gyroscope
Designing 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 mode
Design 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 control
Integrated Guidance and Control Design by Combining Backstepping and Sliding Mode Control Methods [Volume 9, Issue 4, 2016, Pages 39-50]
-
Small satellite
Design and Manufacture of Thermal Model of AUTSAT Satellite and Its Thermal Balance Test [Volume 9, Issue 2, 2016, Pages 61-76]
-
Software in the loop
Design and Implementation of Backstepping-Sliding mode Attitude Controller in The Prossecor in The Loop Test Bed [Volume 9, Issue 1, 2016, Pages 25-35]
-
Sovereignty
Role of States in Regulating Space Activities in International Law [Volume 9, Issue 4, 2016, Pages 27-37]
-
Space activities
Role of States in Regulating Space Activities in International Law [Volume 9, Issue 4, 2016, Pages 27-37]
-
Space boom
Identification of Space Deployable Mechanisms [Volume 9, Issue 3, 2016, Pages 53-71]
-
Spacecraft Deployable antenna
Identification of Space Deployable Mechanisms [Volume 9, Issue 3, 2016, Pages 53-71]
-
Space deployable mechanism
Identification of Space Deployable Mechanisms [Volume 9, Issue 3, 2016, Pages 53-71]
-
Space Inflatable devices
Identification of Space Deployable Mechanisms [Volume 9, Issue 3, 2016, Pages 53-71]
-
Staged combustion
Optimization 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 approach
Using 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
Using 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 law
Designing 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 software
Reduce Position and Velocity RMS Error of Non-linear Filters in LEO Satellite Radar Tracking [Volume 9, Issue 4, 2016, Pages 51-63]
-
Swirl injector
Review 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 Development
Space Launch System Family Technology Development Model from Propulsion Aspect with Cost Approach [Volume 9, Issue 4, 2016, Pages 1-12]
-
Thermal balance test
Design and Manufacture of Thermal Model of AUTSAT Satellite and Its Thermal Balance Test [Volume 9, Issue 2, 2016, Pages 61-76]
-
Thermal model
Design and Manufacture of Thermal Model of AUTSAT Satellite and Its Thermal Balance Test [Volume 9, Issue 2, 2016, Pages 61-76]
-
Thermodynamic cycle
Optimization of Schematic and Parameters of Staged Combustion Launch Vehicle Liquid Engines [Volume 9, Issue 1, 2016, Pages 1-11]
-
Thrust
Review 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 interception
Integrated Guidance and Control Design by Combining Backstepping and Sliding Mode Control Methods [Volume 9, Issue 4, 2016, Pages 39-50]
U
-
Uncertainty and actuator saturation
Satellite 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 saturation
Satellite 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 tests
Design and Fabrication of Spool Type Pin Puller Mechanism- from Concept to Qualification Model [Volume 9, Issue 3, 2016, Pages 37-51]
-
VEGF
The Effects of Simulated Microgravity on Serum Levels of VEGF in Male Wistar Rats [Volume 9, Issue 4, 2016, Pages 63-68]
-
Vibration tests
Design and Fabrication of Spool Type Pin Puller Mechanism- from Concept to Qualification Model [Volume 9, Issue 3, 2016, Pages 37-51]