Journal of Space Science and Technology

Journal of Space Science and Technology

Keyword Index
A
  • Adaptive-neuro-fuzzy controller Design and Real-time Implementation of the Adaptive-Neuro-Fuzzy Controller for a Temperature Control System using Model-Based Design [Volume 10, Issue 4, 2017, Pages 9-17]
  • Amplitude and frequency of oscillation Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 2, 2017, Pages 65-72]
  • Artificial Neural Networks Satellite Orbit Prediction Through Observation Data and the Artificial Neural Networks [Volume 10, Issue 2, 2017, Pages 1-8]
  • Assumption of risk Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 3, 2017, Pages 67-75]
  • Atomization efficiency Extraction of a Theoretical Energy-based Model to Estimate Mean Droplet Diameter of the Swirl Injector Spray [Volume 10, Issue 3, 2017, Pages 59-65]
  • Atomization setup Microscopic Test of a Swirl Injector by High-speed Photography [Volume 10, Issue 4, 2017, Pages 1-7]
  • Attitude control of spacecraft Designing Spacecraft Attitude Control Using Model-free Optimal Control Theory [Volume 10, Issue 3, 2017, Pages 41-57]
  • Attitude determination Sun Vector and Magnetic Vector Simulation for Hardware in the Loop Tests [Volume 10, Issue 1, 2017, Pages 47-53]
  • AZMIN tool A Software for Establishing Technical Specifications of GEO Communication Satellites [Volume 10, Issue 3, 2017, Pages 1-14]
C
  • Combustion efficiency Numerical Simulation of Turbulent Reacting flow in a Trapped Vortex Combustor [Volume 10, Issue 1, 2017, Pages 15-25]
  • Communication satellite HIL Experimental Analyses of Satellite Electrical Power Subsystem (EPS) in De-tumbling Mode [Volume 10, Issue 4, 2017, Pages 19-28]
  • Communication satellites A Software for Establishing Technical Specifications of GEO Communication Satellites [Volume 10, Issue 3, 2017, Pages 1-14]
  • Communication satellites GEO Communication Satellite Engineering Design Code [Volume 10, Issue 4, 2017, Pages 41-54]
  • Container Numerical Simulation of Sloshing in a Container under Translational and Angular Accelerations [Volume 10, Issue 2, 2017, Pages 9-21]
  • Contribution of injured person Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 3, 2017, Pages 67-75]
  • Cyclone Effective Parameters of the Aluminum Particles Cyclone Separator in the Effervescent Fuel [Volume 10, Issue 1, 2017, Pages 35-45]
D
  • Damping baffles Numerical Simulation of Sloshing in a Container under Translational and Angular Accelerations [Volume 10, Issue 2, 2017, Pages 9-21]
  • Decreased design time A Software for Establishing Technical Specifications of GEO Communication Satellites [Volume 10, Issue 3, 2017, Pages 1-14]
  • De-tumbling mode HIL Experimental Analyses of Satellite Electrical Power Subsystem (EPS) in De-tumbling Mode [Volume 10, Issue 4, 2017, Pages 19-28]
  • Differential electrical potential Improvement of the Electrical Potential Distribution on the Surface Geostationary Satellites using Material Change [Volume 10, Issue 3, 2017, Pages 25-39]
  • Differential flatness Flatness-based Near Optimal Guidance [Volume 10, Issue 3, 2017, Pages 15-24]
  • Dual throat nozzle 2D Simulation of Designed Dual Throat Nozzle using Geometrical Analogy [Volume 10, Issue 2, 2017, Pages 23-32]
  • Duty to mitigate Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 3, 2017, Pages 67-75]
  • Dynamic programming Designing Spacecraft Attitude Control Using Model-free Optimal Control Theory [Volume 10, Issue 3, 2017, Pages 41-57]
E
  • Earth station Plasma Antenna Technology in Space Missions [Volume 10, Issue 1, 2017, Pages 27-34]
  • Effervescent fuel Effective Parameters of the Aluminum Particles Cyclone Separator in the Effervescent Fuel [Volume 10, Issue 1, 2017, Pages 35-45]
  • Electricalpower subsystem HIL Experimental Analyses of Satellite Electrical Power Subsystem (EPS) in De-tumbling Mode [Volume 10, Issue 4, 2017, Pages 19-28]
  • Electrostatic discharge Improvement of the Electrical Potential Distribution on the Surface Geostationary Satellites using Material Change [Volume 10, Issue 3, 2017, Pages 25-39]
  • Emission indices Numerical Simulation of Turbulent Reacting flow in a Trapped Vortex Combustor [Volume 10, Issue 1, 2017, Pages 15-25]
  • Energy-based model Extraction of a Theoretical Energy-based Model to Estimate Mean Droplet Diameter of the Swirl Injector Spray [Volume 10, Issue 3, 2017, Pages 59-65]
  • Estimator A Survey on Vision Navigation Methods for UAV Navigation Applications [Volume 10, Issue 2, 2017, Pages 33-52]
  • Experimental data Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 2, 2017, Pages 65-72]
  • Explicit guidance Flatness-based Near Optimal Guidance [Volume 10, Issue 3, 2017, Pages 15-24]
F
  • Floating electrical potential Improvement of the Electrical Potential Distribution on the Surface Geostationary Satellites using Material Change [Volume 10, Issue 3, 2017, Pages 25-39]
G
  • Genetic Algorithm Flatness-based Near Optimal Guidance [Volume 10, Issue 3, 2017, Pages 15-24]
  • Geometrical analogy 2D Simulation of Designed Dual Throat Nozzle using Geometrical Analogy [Volume 10, Issue 2, 2017, Pages 23-32]
  • GEO orbit GEO Communication Satellite Engineering Design Code [Volume 10, Issue 4, 2017, Pages 41-54]
  • Geostationary orbit A Software for Establishing Technical Specifications of GEO Communication Satellites [Volume 10, Issue 3, 2017, Pages 1-14]
H
  • Hardware in loop HIL Experimental Analyses of Satellite Electrical Power Subsystem (EPS) in De-tumbling Mode [Volume 10, Issue 4, 2017, Pages 19-28]
  • Helmholtz coil Sun Vector and Magnetic Vector Simulation for Hardware in the Loop Tests [Volume 10, Issue 1, 2017, Pages 47-53]
  • Hydrazine monopropellant propulsion system Monopropellant Propulsion System Design using Multidisciplinary Design Optimization, Sequential Design Method, and Comparing Results [Volume 10, Issue 2, 2017, Pages 53-63]
I
  • Inertial Navigation System A Survey on Vision Navigation Methods for UAV Navigation Applications [Volume 10, Issue 2, 2017, Pages 33-52]
  • International liability Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 3, 2017, Pages 67-75]
L
  • Launch abort system A Nonlinear Attitude Controller for a Launch Abort System of a Manned Spacecraft [Volume 10, Issue 1, 2017, Pages 1-13]
  • Linear Quadratic Regulator Designing Spacecraft Attitude Control Using Model-free Optimal Control Theory [Volume 10, Issue 3, 2017, Pages 41-57]
  • Liquid sheet instability Microscopic Test of a Swirl Injector by High-speed Photography [Volume 10, Issue 4, 2017, Pages 1-7]
M
  • Magnetometer Sun Vector and Magnetic Vector Simulation for Hardware in the Loop Tests [Volume 10, Issue 1, 2017, Pages 47-53]
  • Mean droplet diameter Extraction of a Theoretical Energy-based Model to Estimate Mean Droplet Diameter of the Swirl Injector Spray [Volume 10, Issue 3, 2017, Pages 59-65]
  • Micro-turbine 2D Simulation of Designed Dual Throat Nozzle using Geometrical Analogy [Volume 10, Issue 2, 2017, Pages 23-32]
  • Model-based design Design and Real-time Implementation of the Adaptive-Neuro-Fuzzy Controller for a Temperature Control System using Model-Based Design [Volume 10, Issue 4, 2017, Pages 9-17]
  • Model-Free controller Designing Spacecraft Attitude Control Using Model-free Optimal Control Theory [Volume 10, Issue 3, 2017, Pages 41-57]
  • Multi beam satellite communication systems An Optimal Power Allocation in Multi-Beam Satellite Communication Systems Including Inter-Beam Interference by Particle Swarm Optimization (PSO) [Volume 10, Issue 1, 2017, Pages 55-60]
  • Multidisciplinary design optimization Monopropellant Propulsion System Design using Multidisciplinary Design Optimization, Sequential Design Method, and Comparing Results [Volume 10, Issue 2, 2017, Pages 53-63]
N
  • Nonlinear attitude Control A Nonlinear Attitude Controller for a Launch Abort System of a Manned Spacecraft [Volume 10, Issue 1, 2017, Pages 1-13]
  • Nonlinear Quadratic Tracking (NQT) Robust Guidance Algorithmfor Reentry Vehicles based on PLS Regression in the Presence ofInitail Parameter Uncertainties [Volume 10, Issue 4, 2017, Pages 29-40]
  • Non-linear sloshing Numerical Simulation of Sloshing in a Container under Translational and Angular Accelerations [Volume 10, Issue 2, 2017, Pages 9-21]
  • Numerical analysis Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 2, 2017, Pages 65-72]
O
  • On-off thruster actuator Robust Optimization of Satellite Attitude Control with Thruster Actuators based on Combined Objective Function [Volume 10, Issue 4, 2017, Pages 55-66]
  • Optimal guidance Flatness-based Near Optimal Guidance [Volume 10, Issue 3, 2017, Pages 15-24]
  • Optimal guidance Robust Guidance Algorithmfor Reentry Vehicles based on PLS Regression in the Presence ofInitail Parameter Uncertainties [Volume 10, Issue 4, 2017, Pages 29-40]
P
  • Parametric models GEO Communication Satellite Engineering Design Code [Volume 10, Issue 4, 2017, Pages 41-54]
  • Partial Least Squares (PLS) Robust Guidance Algorithmfor Reentry Vehicles based on PLS Regression in the Presence ofInitail Parameter Uncertainties [Volume 10, Issue 4, 2017, Pages 29-40]
  • Plasma antenna Plasma Antenna Technology in Space Missions [Volume 10, Issue 1, 2017, Pages 27-34]
  • Plasma array Plasma Antenna Technology in Space Missions [Volume 10, Issue 1, 2017, Pages 27-34]
  • Power allocation An Optimal Power Allocation in Multi-Beam Satellite Communication Systems Including Inter-Beam Interference by Particle Swarm Optimization (PSO) [Volume 10, Issue 1, 2017, Pages 55-60]
  • PSO optimization An Optimal Power Allocation in Multi-Beam Satellite Communication Systems Including Inter-Beam Interference by Particle Swarm Optimization (PSO) [Volume 10, Issue 1, 2017, Pages 55-60]
R
  • Reacting turbulent flow Numerical Simulation of Turbulent Reacting flow in a Trapped Vortex Combustor [Volume 10, Issue 1, 2017, Pages 15-25]
  • Reentry Flatness-based Near Optimal Guidance [Volume 10, Issue 3, 2017, Pages 15-24]
  • Re-entry vehicles Robust Guidance Algorithmfor Reentry Vehicles based on PLS Regression in the Presence ofInitail Parameter Uncertainties [Volume 10, Issue 4, 2017, Pages 29-40]
  • Regression Robust Guidance Algorithmfor Reentry Vehicles based on PLS Regression in the Presence ofInitail Parameter Uncertainties [Volume 10, Issue 4, 2017, Pages 29-40]
  • Resonance Numerical Simulation of Sloshing in a Container under Translational and Angular Accelerations [Volume 10, Issue 2, 2017, Pages 9-21]
  • Robustguidance Robust Guidance Algorithmfor Reentry Vehicles based on PLS Regression in the Presence ofInitail Parameter Uncertainties [Volume 10, Issue 4, 2017, Pages 29-40]
  • Roll damping coefficient Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 2, 2017, Pages 65-72]
S
  • Satellite attitude control Robust Optimization of Satellite Attitude Control with Thruster Actuators based on Combined Objective Function [Volume 10, Issue 4, 2017, Pages 55-66]
  • Satellite Position Satellite Orbit Prediction Through Observation Data and the Artificial Neural Networks [Volume 10, Issue 2, 2017, Pages 1-8]
  • Separation Effective Parameters of the Aluminum Particles Cyclone Separator in the Effervescent Fuel [Volume 10, Issue 1, 2017, Pages 35-45]
  • Sequential design Monopropellant Propulsion System Design using Multidisciplinary Design Optimization, Sequential Design Method, and Comparing Results [Volume 10, Issue 2, 2017, Pages 53-63]
  • Spacecraft Plasma Antenna Technology in Space Missions [Volume 10, Issue 1, 2017, Pages 27-34]
  • Spacecraft A Nonlinear Attitude Controller for a Launch Abort System of a Manned Spacecraft [Volume 10, Issue 1, 2017, Pages 1-13]
  • Spacecraft charging Improvement of the Electrical Potential Distribution on the Surface Geostationary Satellites using Material Change [Volume 10, Issue 3, 2017, Pages 25-39]
  • Space law Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 3, 2017, Pages 67-75]
  • SPIS Improvement of the Electrical Potential Distribution on the Surface Geostationary Satellites using Material Change [Volume 10, Issue 3, 2017, Pages 25-39]
  • Spray cone Microscopic Test of a Swirl Injector by High-speed Photography [Volume 10, Issue 4, 2017, Pages 1-7]
  • Statistical design A Software for Establishing Technical Specifications of GEO Communication Satellites [Volume 10, Issue 3, 2017, Pages 1-14]
  • Statistical models GEO Communication Satellite Engineering Design Code [Volume 10, Issue 4, 2017, Pages 41-54]
  • Sun sensor Sun Vector and Magnetic Vector Simulation for Hardware in the Loop Tests [Volume 10, Issue 1, 2017, Pages 47-53]
  • Sun simulator Sun Vector and Magnetic Vector Simulation for Hardware in the Loop Tests [Volume 10, Issue 1, 2017, Pages 47-53]
  • Swirl injector Extraction of a Theoretical Energy-based Model to Estimate Mean Droplet Diameter of the Swirl Injector Spray [Volume 10, Issue 3, 2017, Pages 59-65]
  • Swirl injector Microscopic Test of a Swirl Injector by High-speed Photography [Volume 10, Issue 4, 2017, Pages 1-7]
T
  • Temperature control system Design and Real-time Implementation of the Adaptive-Neuro-Fuzzy Controller for a Temperature Control System using Model-Based Design [Volume 10, Issue 4, 2017, Pages 9-17]
  • Thrust vector control 2D Simulation of Designed Dual Throat Nozzle using Geometrical Analogy [Volume 10, Issue 2, 2017, Pages 23-32]
  • Time step Investigating the Effective Numerical Solution Parameters in Calculating the Roll Damping Coefficient [Volume 10, Issue 2, 2017, Pages 65-72]
  • TLE Satellite Orbit Prediction Through Observation Data and the Artificial Neural Networks [Volume 10, Issue 2, 2017, Pages 1-8]
  • Trapped vortex combustor Numerical Simulation of Turbulent Reacting flow in a Trapped Vortex Combustor [Volume 10, Issue 1, 2017, Pages 15-25]
  • Turbulent Flow Effective Parameters of the Aluminum Particles Cyclone Separator in the Effervescent Fuel [Volume 10, Issue 1, 2017, Pages 35-45]
  • Two phase Effective Parameters of the Aluminum Particles Cyclone Separator in the Effervescent Fuel [Volume 10, Issue 1, 2017, Pages 35-45]
U
  • UAV A Survey on Vision Navigation Methods for UAV Navigation Applications [Volume 10, Issue 2, 2017, Pages 33-52]
  • Uncertainty Robust Guidance Algorithmfor Reentry Vehicles based on PLS Regression in the Presence ofInitail Parameter Uncertainties [Volume 10, Issue 4, 2017, Pages 29-40]
  • Uncertainty Robust Optimization of Satellite Attitude Control with Thruster Actuators based on Combined Objective Function [Volume 10, Issue 4, 2017, Pages 55-66]
V
  • Validation GEO Communication Satellite Engineering Design Code [Volume 10, Issue 4, 2017, Pages 41-54]
  • Vision Navigation A Survey on Vision Navigation Methods for UAV Navigation Applications [Volume 10, Issue 2, 2017, Pages 33-52]
  • Volume of fluid technique Numerical Simulation of Sloshing in a Container under Translational and Angular Accelerations [Volume 10, Issue 2, 2017, Pages 9-21]
W
  • Weber number Extraction of a Theoretical Energy-based Model to Estimate Mean Droplet Diameter of the Swirl Injector Spray [Volume 10, Issue 3, 2017, Pages 59-65]