A
-
Adaptive sliding mode control
Attitude Control System Design Based on Fluidic Momentum Controllers under Adaptive Sliding Mode [Volume 7, Issue 2, 2014]
-
Aerodynamic heating
Laminar and Turbulent Aero Heating Predictions over Blunt Body in Hypersonic Flow [Volume 7, Issue 1, 2014]
-
Aerodynamic heating
Approximate Viscous Shock-Layer Analysis of Axisymmetric Bodies in Perfect Gas Hypersonic Flow [Volume 7, Issue 1, 2014]
-
Agile satellite
Design, Manufacturing and Test of a Three Degrees-of-Freedom Attitude Control Simulator for an Agile Micro-Satellite Based on Single Gimbal Control Moment Gyros [Volume 7, Issue 3, 2014]
-
Agility satellite
Attitude Stabilization and Manauvring of Agility Nanosatellite with Control Moment Gyros [Volume 7, Issue 2, 2014]
-
Air bearing
Design, Manufacturing and Test of a Three Degrees-of-Freedom Attitude Control Simulator for an Agile Micro-Satellite Based on Single Gimbal Control Moment Gyros [Volume 7, Issue 3, 2014]
-
Airspace
Passage of Space Objects over the Territory of States from the Perspective of the International Law [Volume 7, Issue 3, 2014]
-
Altitude
Effects of Some Parameters on Thermal Control of a LEO Satellite [Volume 7, Issue 1, 2014]
-
Approximate
Approximate Viscous Shock-Layer Analysis of Axisymmetric Bodies in Perfect Gas Hypersonic Flow [Volume 7, Issue 1, 2014]
-
Artificial Neural Network
Verification of a Low Cost Method for Accelerometers Calibration with a Two-Axis Table [Volume 7, Issue 4, 2014]
-
Artifitialintelligence
Intelligent Satellite Orbit Prediction Based on Time Series Analysis [Volume 7, Issue 3, 2014]
-
Ascend phase
Ascending Phase Fuzzy Logic Guidance of Satellite Launch Vehicles for Reducing the Adverse Wind Effects [Volume 7, Issue 3, 2014]
-
Attitude control
Design, Manufacturing and Test of a Three Degrees-of-Freedom Attitude Control Simulator for an Agile Micro-Satellite Based on Single Gimbal Control Moment Gyros [Volume 7, Issue 3, 2014]
B
-
Board Processing
FPGA Implementation of JPEG and JPEG2000-Based Dynamic Partial Reconfiguration on SOC for Remote Sensing Satellite On-Board Processing [Volume 7, Issue 1, 2014]
C
-
Calibration
Verification of a Low Cost Method for Accelerometers Calibration with a Two-Axis Table [Volume 7, Issue 4, 2014]
-
Caspian Sea
Empirical Modeling of Clarity in the Caspian Sea using MERIS Data [Volume 7, Issue 2, 2014]
-
Clarity model
Empirical Modeling of Clarity in the Caspian Sea using MERIS Data [Volume 7, Issue 2, 2014]
-
Code design
Comprehensive Code of Remote Sensing Satellite Conceptual Design [Volume 7, Issue 2, 2014]
-
Collaborative design
Integrated Design of Orbital Transfer Block in an Optimized and Multistep Converged Environment [Volume 7, Issue 4, 2014]
-
Conceptual design
Comprehensive Code of Remote Sensing Satellite Conceptual Design [Volume 7, Issue 2, 2014]
-
Conceptual design
Comprehensive Pattern in Designing Low-Thrust Space Propulsion Systems [Volume 7, Issue 3, 2014]
-
Control
Fuzzy Sliding Mode for Spacecraft Formation Control in Eccentric Orbits [Volume 7, Issue 1, 2014]
-
Control Moment Gyroscope (CMG)
Attitude Stabilization and Manauvring of Agility Nanosatellite with Control Moment Gyros [Volume 7, Issue 2, 2014]
D
-
D
Attitude Control of Spacecraft by State Dependent Riccati Equation and Power Series Expansion of Riccati Methods [Volume 7, Issue 4, 2014]
-
Delicate equipments
Isolation of Satellite's Sensitive Equipments from Longitudinal Vibration of Launch Vehicle Using Silicone Gel [Volume 7, Issue 4, 2014]
-
Design optimization
Satellite Conceptual Design Multi-Objective Optimization Using Co Framework [Volume 7, Issue 1, 2014]
-
Diagnostic indication
Neural Network Based Diagnostic Indication of a Liquid Propellant Engine with Faulty Data Collection System [Volume 7, Issue 2, 2014]
-
Drogue chute
Study of Recovery System Performance of a Sounding Rocket using Launching Tests [Volume 7, Issue 2, 2014]
E
-
Edge detection
Automatic Reading of a Trade Gyrocompass Using Image Processing and Neural Networks [Volume 7, Issue 2, 2014]
-
Experimental analysis
Experimental Analysis of Pyroshock Wave Propagation in Kavoshgar's Payload [Volume 7, Issue 4, 2014]
F
-
Faulty data collection system
Neural Network Based Diagnostic Indication of a Liquid Propellant Engine with Faulty Data Collection System [Volume 7, Issue 2, 2014]
-
Finite element method
Isolation of Satellite's Sensitive Equipments from Longitudinal Vibration of Launch Vehicle Using Silicone Gel [Volume 7, Issue 4, 2014]
-
Firstorder metod
Second Order Level Set Method in Numerical Simulation of the Grain Burn-Back [Volume 7, Issue 3, 2014]
-
Flow Field
Laminar and Turbulent Aero Heating Predictions over Blunt Body in Hypersonic Flow [Volume 7, Issue 1, 2014]
-
Fluidic Momentum Controller (FMC)
Attitude Control System Design Based on Fluidic Momentum Controllers under Adaptive Sliding Mode [Volume 7, Issue 2, 2014]
-
FMEA
Reliability Determination of a Sounding Rocket Separation System Using its Reliability Block Diagram and FMEA [Volume 7, Issue 1, 2014]
-
Fuzzy
Fuzzy Sliding Mode for Spacecraft Formation Control in Eccentric Orbits [Volume 7, Issue 1, 2014]
-
Fuzzy guidance
Ascending Phase Fuzzy Logic Guidance of Satellite Launch Vehicles for Reducing the Adverse Wind Effects [Volume 7, Issue 3, 2014]
-
Fuzzy logic
Precise Positioning in GPS Receivers for Very High Velocities Using Combination of Recursive Least Squares and Fuzzy Logic [Volume 7, Issue 4, 2014]
G
-
Genetic Algorithms
Satellite Conceptual Design Multi-Objective Optimization Using Co Framework [Volume 7, Issue 1, 2014]
-
Genetic heuristic optimization algorithm
Extracting the Non-ObservableStates in Alignment & Calibration Process for Gimballed Inertial Navigation Systems [Volume 7, Issue 3, 2014]
-
Geostationary orbit
Analytical Solution to Relative Motion Dynamics in Satellite Formation Flying Using Geostationary Orbit Sets [Volume 7, Issue 4, 2014]
-
Gimballed
Extracting the Non-ObservableStates in Alignment & Calibration Process for Gimballed Inertial Navigation Systems [Volume 7, Issue 3, 2014]
-
Grain burn
Second Order Level Set Method in Numerical Simulation of the Grain Burn-Back [Volume 7, Issue 3, 2014]
H
-
Hamiltonian
Attitude Control of Spacecraft by State Dependent Riccati Equation and Power Series Expansion of Riccati Methods [Volume 7, Issue 4, 2014]
-
Hypersonic Flow
Laminar and Turbulent Aero Heating Predictions over Blunt Body in Hypersonic Flow [Volume 7, Issue 1, 2014]
-
HypersonicFlow
Approximate Viscous Shock-Layer Analysis of Axisymmetric Bodies in Perfect Gas Hypersonic Flow [Volume 7, Issue 1, 2014]
I
-
Inertial Navigation
Extracting the Non-ObservableStates in Alignment & Calibration Process for Gimballed Inertial Navigation Systems [Volume 7, Issue 3, 2014]
-
Inflation
Study of Recovery System Performance of a Sounding Rocket using Launching Tests [Volume 7, Issue 2, 2014]
-
Initial alignment
Extracting the Non-ObservableStates in Alignment & Calibration Process for Gimballed Inertial Navigation Systems [Volume 7, Issue 3, 2014]
-
Innocent passage
Passage of Space Objects over the Territory of States from the Perspective of the International Law [Volume 7, Issue 3, 2014]
-
Integration
Integrated Design of Orbital Transfer Block in an Optimized and Multistep Converged Environment [Volume 7, Issue 4, 2014]
K
-
Kavoshgar payload
Experimental Analysis of Pyroshock Wave Propagation in Kavoshgar's Payload [Volume 7, Issue 4, 2014]
L
-
Laminar Flow
Laminar and Turbulent Aero Heating Predictions over Blunt Body in Hypersonic Flow [Volume 7, Issue 1, 2014]
-
Launching test
Study of Recovery System Performance of a Sounding Rocket using Launching Tests [Volume 7, Issue 2, 2014]
-
Launch Vehicle
Ascending Phase Fuzzy Logic Guidance of Satellite Launch Vehicles for Reducing the Adverse Wind Effects [Volume 7, Issue 3, 2014]
-
Learning vector quantization
Automatic Reading of a Trade Gyrocompass Using Image Processing and Neural Networks [Volume 7, Issue 2, 2014]
-
Level set
Second Order Level Set Method in Numerical Simulation of the Grain Burn-Back [Volume 7, Issue 3, 2014]
-
Liquid Propellant Engine
Neural Network Based Diagnostic Indication of a Liquid Propellant Engine with Faulty Data Collection System [Volume 7, Issue 2, 2014]
-
Liquid Propellant Engine
Comprehensive Pattern in Designing Low-Thrust Space Propulsion Systems [Volume 7, Issue 3, 2014]
-
Longitudinal vibrations
Isolation of Satellite's Sensitive Equipments from Longitudinal Vibration of Launch Vehicle Using Silicone Gel [Volume 7, Issue 4, 2014]
-
Low
Comprehensive Pattern in Designing Low-Thrust Space Propulsion Systems [Volume 7, Issue 3, 2014]
-
LQG/LQR
Attitude Stabilization and Manauvring of Agility Nanosatellite with Control Moment Gyros [Volume 7, Issue 2, 2014]
M
-
Main parachute
Study of Recovery System Performance of a Sounding Rocket using Launching Tests [Volume 7, Issue 2, 2014]
-
MERIS
Empirical Modeling of Clarity in the Caspian Sea using MERIS Data [Volume 7, Issue 2, 2014]
-
Microelectro mechanical accelerometers
Verification of a Low Cost Method for Accelerometers Calibration with a Two-Axis Table [Volume 7, Issue 4, 2014]
-
Motion analysis
Automatic Reading of a Trade Gyrocompass Using Image Processing and Neural Networks [Volume 7, Issue 2, 2014]
-
Multilayer Perceptron
Automatic Reading of a Trade Gyrocompass Using Image Processing and Neural Networks [Volume 7, Issue 2, 2014]
N
-
Navigation equations solving
Precise Positioning in GPS Receivers for Very High Velocities Using Combination of Recursive Least Squares and Fuzzy Logic [Volume 7, Issue 4, 2014]
-
Neural Network
Neural Network Based Diagnostic Indication of a Liquid Propellant Engine with Faulty Data Collection System [Volume 7, Issue 2, 2014]
-
Nonlinear optimal control
Attitude Control of Spacecraft by State Dependent Riccati Equation and Power Series Expansion of Riccati Methods [Volume 7, Issue 4, 2014]
O
-
Opening force
Study of Recovery System Performance of a Sounding Rocket using Launching Tests [Volume 7, Issue 2, 2014]
-
Optimized environment
Integrated Design of Orbital Transfer Block in an Optimized and Multistep Converged Environment [Volume 7, Issue 4, 2014]
-
Orbital position
Intelligent Satellite Orbit Prediction Based on Time Series Analysis [Volume 7, Issue 3, 2014]
-
Outer space
Passage of Space Objects over the Territory of States from the Perspective of the International Law [Volume 7, Issue 3, 2014]
P
-
Parallel boosters
Investigation of Length and Velocity Variation Effects on Unsteady Separation of Parallel Boosters [Volume 7, Issue 2, 2014]
-
Perfect Gas
Approximate Viscous Shock-Layer Analysis of Axisymmetric Bodies in Perfect Gas Hypersonic Flow [Volume 7, Issue 1, 2014]
-
Pyroshock
Experimental Analysis of Pyroshock Wave Propagation in Kavoshgar's Payload [Volume 7, Issue 4, 2014]
-
Pyrotechnic material
Experimental Analysis of Pyroshock Wave Propagation in Kavoshgar's Payload [Volume 7, Issue 4, 2014]
Q
-
Quadratic regulator
Attitude Control of Spacecraft by State Dependent Riccati Equation and Power Series Expansion of Riccati Methods [Volume 7, Issue 4, 2014]
R
-
Reconfigurable
FPGA Implementation of JPEG and JPEG2000-Based Dynamic Partial Reconfiguration on SOC for Remote Sensing Satellite On-Board Processing [Volume 7, Issue 1, 2014]
-
Recovery
Study of Recovery System Performance of a Sounding Rocket using Launching Tests [Volume 7, Issue 2, 2014]
-
Recursive least squares
Precise Positioning in GPS Receivers for Very High Velocities Using Combination of Recursive Least Squares and Fuzzy Logic [Volume 7, Issue 4, 2014]
-
Relative position
Analytical Solution to Relative Motion Dynamics in Satellite Formation Flying Using Geostationary Orbit Sets [Volume 7, Issue 4, 2014]
-
Relative velocity
Analytical Solution to Relative Motion Dynamics in Satellite Formation Flying Using Geostationary Orbit Sets [Volume 7, Issue 4, 2014]
-
Remote Sensing
Remote Sensing Role in Land Use StudiesCase Study: Tehran Metropolitan and its Boundary [Volume 7, Issue 3, 2014]
-
Required velocity
Implicit Guidance Equations in Polar Coordinates [Volume 7, Issue 4, 2014]
S
-
Satellite attitude control
Attitude Stabilization and Manauvring of Agility Nanosatellite with Control Moment Gyros [Volume 7, Issue 2, 2014]
-
Satellite attitude control
Attitude Control System Design Based on Fluidic Momentum Controllers under Adaptive Sliding Mode [Volume 7, Issue 2, 2014]
-
Satellite formation flying
Analytical Solution to Relative Motion Dynamics in Satellite Formation Flying Using Geostationary Orbit Sets [Volume 7, Issue 4, 2014]
-
Satelliteimage
Remote Sensing Role in Land Use StudiesCase Study: Tehran Metropolitan and its Boundary [Volume 7, Issue 3, 2014]
-
Satellite remote sensing
Comprehensive Code of Remote Sensing Satellite Conceptual Design [Volume 7, Issue 2, 2014]
-
Secchi depth
Empirical Modeling of Clarity in the Caspian Sea using MERIS Data [Volume 7, Issue 2, 2014]
-
Second order metod
Second Order Level Set Method in Numerical Simulation of the Grain Burn-Back [Volume 7, Issue 3, 2014]
-
Separation
Investigation of Length and Velocity Variation Effects on Unsteady Separation of Parallel Boosters [Volume 7, Issue 2, 2014]
-
Shock response spectrum
Experimental Analysis of Pyroshock Wave Propagation in Kavoshgar's Payload [Volume 7, Issue 4, 2014]
-
Silicone gel
Isolation of Satellite's Sensitive Equipments from Longitudinal Vibration of Launch Vehicle Using Silicone Gel [Volume 7, Issue 4, 2014]
-
Simulation
Comprehensive Code of Remote Sensing Satellite Conceptual Design [Volume 7, Issue 2, 2014]
-
Single
Design, Manufacturing and Test of a Three Degrees-of-Freedom Attitude Control Simulator for an Agile Micro-Satellite Based on Single Gimbal Control Moment Gyros [Volume 7, Issue 3, 2014]
-
Singularity condition
Attitude Stabilization and Manauvring of Agility Nanosatellite with Control Moment Gyros [Volume 7, Issue 2, 2014]
-
Sliding mode
Fuzzy Sliding Mode for Spacecraft Formation Control in Eccentric Orbits [Volume 7, Issue 1, 2014]
-
Sounding rocket
Study of Recovery System Performance of a Sounding Rocket using Launching Tests [Volume 7, Issue 2, 2014]
-
Sovereignty
Passage of Space Objects over the Territory of States from the Perspective of the International Law [Volume 7, Issue 3, 2014]
-
Space objects
Passage of Space Objects over the Territory of States from the Perspective of the International Law [Volume 7, Issue 3, 2014]
-
State dependent riccati equation
Attitude Control of Spacecraft by State Dependent Riccati Equation and Power Series Expansion of Riccati Methods [Volume 7, Issue 4, 2014]
-
Steering of CMG
Attitude Stabilization and Manauvring of Agility Nanosatellite with Control Moment Gyros [Volume 7, Issue 2, 2014]
T
-
Tehran
Remote Sensing Role in Land Use StudiesCase Study: Tehran Metropolitan and its Boundary [Volume 7, Issue 3, 2014]
-
Thrust
Comprehensive Pattern in Designing Low-Thrust Space Propulsion Systems [Volume 7, Issue 3, 2014]
-
Thruster
Comprehensive Pattern in Designing Low-Thrust Space Propulsion Systems [Volume 7, Issue 3, 2014]
-
Time Processing
FPGA Implementation of JPEG and JPEG2000-Based Dynamic Partial Reconfiguration on SOC for Remote Sensing Satellite On-Board Processing [Volume 7, Issue 1, 2014]
-
TLE
Intelligent Satellite Orbit Prediction Based on Time Series Analysis [Volume 7, Issue 3, 2014]
-
Turbulent Flow
Laminar and Turbulent Aero Heating Predictions over Blunt Body in Hypersonic Flow [Volume 7, Issue 1, 2014]
-
Two
Verification of a Low Cost Method for Accelerometers Calibration with a Two-Axis Table [Volume 7, Issue 4, 2014]
U
-
UDF
Investigation of Length and Velocity Variation Effects on Unsteady Separation of Parallel Boosters [Volume 7, Issue 2, 2014]
-
Uncertainly
Attitude Control System Design Based on Fluidic Momentum Controllers under Adaptive Sliding Mode [Volume 7, Issue 2, 2014]
-
Univariate regression
Empirical Modeling of Clarity in the Caspian Sea using MERIS Data [Volume 7, Issue 2, 2014]
V
-
Very high velocities
Precise Positioning in GPS Receivers for Very High Velocities Using Combination of Recursive Least Squares and Fuzzy Logic [Volume 7, Issue 4, 2014]
-
Vibrationisolation
Isolation of Satellite's Sensitive Equipments from Longitudinal Vibration of Launch Vehicle Using Silicone Gel [Volume 7, Issue 4, 2014]
W
-
Wind effect
Ascending Phase Fuzzy Logic Guidance of Satellite Launch Vehicles for Reducing the Adverse Wind Effects [Volume 7, Issue 3, 2014]