Journal of Space Science and Technology

Journal of Space Science and Technology

Keyword Index
A
  • Acoustic oscillations-Methane flame Numerical Investigation of Laminar Premixed Conical Flame Response to Acoustic Excitation [Volume 8, Issue 1, 2015, Pages 9-18]
  • Actuator Saturation Optimal Control of a Flexible Spacecraft in a Proximity Operation Using State Dependent Riccati Equation Approach [Volume 8, Issue 1, 2015, Pages 27-41]
  • Adaptive controller Guidance and Control for Space Capsule in the Presence of Uncertain Dynamic Parameters during the Atmospheric Entry Phase [Volume 8, Issue 3, 2015, Pages 1-13]
  • Aerodynamic heating Aerodynamic Heating Prediction of Flying Body Using Fluid-Solid Conjugate Heat Transfer [Volume 8, Issue 3, 2015, Pages 41-53]
  • Aerodynamic parameter uncertainty Guidance and Control for Space Capsule in the Presence of Uncertain Dynamic Parameters during the Atmospheric Entry Phase [Volume 8, Issue 3, 2015, Pages 1-13]
  • Aided inertial navigation system INS Alignment Improvement Using Rest Heading and Zero-Velocity Updates [Volume 8, Issue 4, 2015, Pages 45-51]
  • Alignment INS Alignment Improvement Using Rest Heading and Zero-Velocity Updates [Volume 8, Issue 4, 2015, Pages 45-51]
  • Artificial Neural Network Improving DGPS Accuracy Using Predictions of Reference Position Components Error Factors [Volume 8, Issue 2, 2015, Pages 41-56]
  • Atmospheric entry phase Guidance and Control for Space Capsule in the Presence of Uncertain Dynamic Parameters during the Atmospheric Entry Phase [Volume 8, Issue 3, 2015, Pages 1-13]
  • Attitude control Design and Manufacturing of a Variable Speed Control Moment Gyro for an Agile Micro-Satellite Attitude Control Simulator [Volume 8, Issue 1, 2015, Pages 73-77]
  • Attitude control Design and Implementation of Attitude Control Systemof a satellite with Stereo-Imaging Scenario in Hardware in the Loop Test Bed [Volume 8, Issue 3, 2015, Pages 15-26]
  • Autoregressive –moving Improving DGPS Accuracy Using Predictions of Reference Position Components Error Factors [Volume 8, Issue 2, 2015, Pages 41-56]
B
  • Boundary Layer Equilibrium Effects on the Hypersonic Laminar Boundary Layer Flow over Axisymmetric Bodies [Volume 8, Issue 4, 2015, Pages 19-27]
C
  • Chattering A New Backstepping Sliding Mode Guidance Law Considering Control Loop Dynamics [Volume 8, Issue 4, 2015, Pages 9-17]
  • Collaborative design Solid Fuel Orbiter Designe in Optimized Space Transfer [Volume 8, Issue 1, 2015, Pages 53-60]
  • Collinear condition Comparison of Direct and Indirect Georeferencing Methods Using Satellite Linear Array Iimages [Volume 8, Issue 2, 2015, Pages 1-10]
  • Combustion instability-Laminar flame Numerical Investigation of Laminar Premixed Conical Flame Response to Acoustic Excitation [Volume 8, Issue 1, 2015, Pages 9-18]
  • Conceptual design Complementary Method the Conceptual Design of Space Craft Electrical Power  Subsystem [Volume 8, Issue 3, 2015, Pages 55-63]
  • Conjugate Gradient Method Hot Air Gun Identification by Inverse Heat Transfer [Volume 8, Issue 4, 2015, Pages 29-34]
  • Conjugate heat transfer Aerodynamic Heating Prediction of Flying Body Using Fluid-Solid Conjugate Heat Transfer [Volume 8, Issue 3, 2015, Pages 41-53]
  • Control loop New Satellite Automatic Tracking by Doppler [Volume 8, Issue 2, 2015, Pages 57-65]
  • Control loop dynamics A New Backstepping Sliding Mode Guidance Law Considering Control Loop Dynamics [Volume 8, Issue 4, 2015, Pages 9-17]
  • Cost Function Online Optimal Integrated Guidance and Control Algorithm Design for Launch Vehicle [Volume 8, Issue 2, 2015, Pages 67-78]
D
  • Differentials global positioning system Improving DGPS Accuracy Using Predictions of Reference Position Components Error Factors [Volume 8, Issue 2, 2015, Pages 41-56]
  • Direct geometric correction method Comparison of Direct and Indirect Georeferencing Methods Using Satellite Linear Array Iimages [Volume 8, Issue 2, 2015, Pages 1-10]
  • Disturbance Optimal Control of a Flexible Spacecraft in a Proximity Operation Using State Dependent Riccati Equation Approach [Volume 8, Issue 1, 2015, Pages 27-41]
  • Doppler frequency New Satellite Automatic Tracking by Doppler [Volume 8, Issue 2, 2015, Pages 57-65]
  • Dynamic sliding mode Dynamic Terminal Sliding Mode Control for an Aerospace Launch Vehicle [Volume 8, Issue 4, 2015, Pages 1-7]
E
  • Effective emissivity Evaluation of Effective Emissivity of a Multilayer Insulation Blanket Using Test [Volume 8, Issue 1, 2015, Pages 19-25]
  • Eigenvectors of the hamiltonian matrix Nonlinear Optimal Control of Space Docking and Rendezvous Problem [Volume 8, Issue 3, 2015, Pages 27-40]
  • Equilibrium air Equilibrium Effects on the Hypersonic Laminar Boundary Layer Flow over Axisymmetric Bodies [Volume 8, Issue 4, 2015, Pages 19-27]
  • Escobal method Effect of Time Separation between Observations on Angles-only Preliminary Orbit Determination [Volume 8, Issue 2, 2015, Pages 19-26]
F
  • Fault tolerantcontrol Nonlinear Dynamic Inversion Fault Tolerant Control for Spacecraft    [Volume 8, Issue 2, 2015, Pages 11-17]
  • Finite-time convergence Dynamic Terminal Sliding Mode Control for an Aerospace Launch Vehicle [Volume 8, Issue 4, 2015, Pages 1-7]
  • Finite-time stabilization New Approach in Guidance Law Design Based on Finite-Time Partial Stability Theorem [Volume 8, Issue 1, 2015, Pages 1-7]
  • Flexible Design a μ-Controller ToControl Attitude of a Flexible Microsatellite [Volume 8, Issue 1, 2015, Pages 61-71]
  • Flexible satellite Active Control of a Smart Satellite under Thermal Loading [Volume 8, Issue 1, 2015, Pages 43-51]
  • Forced Convection Hot Air Gun Identification by Inverse Heat Transfer [Volume 8, Issue 4, 2015, Pages 29-34]
G
  • Gauss method Effect of Time Separation between Observations on Angles-only Preliminary Orbit Determination [Volume 8, Issue 2, 2015, Pages 19-26]
  • Genetic Algorithm Improving DGPS Accuracy Using Predictions of Reference Position Components Error Factors [Volume 8, Issue 2, 2015, Pages 41-56]
  • Georeferencing Comparison of Direct and Indirect Georeferencing Methods Using Satellite Linear Array Iimages [Volume 8, Issue 2, 2015, Pages 1-10]
  • Gradient based algorithms Combining Gradient and Evolutionary Algorithms for Improving Collaborative Optimization Performance [Volume 8, Issue 2, 2015, Pages 27-39]
  • Ground control point Comparison of Direct and Indirect Georeferencing Methods Using Satellite Linear Array Iimages [Volume 8, Issue 2, 2015, Pages 1-10]
  • Guidance law New Approach in Guidance Law Design Based on Finite-Time Partial Stability Theorem [Volume 8, Issue 1, 2015, Pages 1-7]
  • Guidance law A New Backstepping Sliding Mode Guidance Law Considering Control Loop Dynamics [Volume 8, Issue 4, 2015, Pages 9-17]
H
  • Hardware in the loop Design and Implementation of Attitude Control Systemof a satellite with Stereo-Imaging Scenario in Hardware in the Loop Test Bed [Volume 8, Issue 3, 2015, Pages 15-26]
  • Hypersonic Flow Equilibrium Effects on the Hypersonic Laminar Boundary Layer Flow over Axisymmetric Bodies [Volume 8, Issue 4, 2015, Pages 19-27]
I
  • Indirect geometric correction method Comparison of Direct and Indirect Georeferencing Methods Using Satellite Linear Array Iimages [Volume 8, Issue 2, 2015, Pages 1-10]
  • INS INS Alignment Improvement Using Rest Heading and Zero-Velocity Updates [Volume 8, Issue 4, 2015, Pages 45-51]
  • Integral matrix method Equilibrium Effects on the Hypersonic Laminar Boundary Layer Flow over Axisymmetric Bodies [Volume 8, Issue 4, 2015, Pages 19-27]
  • Integrated guidance and control Online Optimal Integrated Guidance and Control Algorithm Design for Launch Vehicle [Volume 8, Issue 2, 2015, Pages 67-78]
  • Inverse Heat Transfer Hot Air Gun Identification by Inverse Heat Transfer [Volume 8, Issue 4, 2015, Pages 29-34]
K
  • Kalman Filter INS Alignment Improvement Using Rest Heading and Zero-Velocity Updates [Volume 8, Issue 4, 2015, Pages 45-51]
L
  • Laplace method Effect of Time Separation between Observations on Angles-only Preliminary Orbit Determination [Volume 8, Issue 2, 2015, Pages 19-26]
  • LQR Optimal Control of a Tri-axial Spacecraft Simulator Test bed Actuated by Reaction Wheels [Volume 8, Issue 4, 2015, Pages 35-44]
M
  • Multidisciplinary design optimization Combining Gradient and Evolutionary Algorithms for Improving Collaborative Optimization Performance [Volume 8, Issue 2, 2015, Pages 27-39]
  • Multilayer insulations Evaluation of Effective Emissivity of a Multilayer Insulation Blanket Using Test [Volume 8, Issue 1, 2015, Pages 19-25]
  • Multiplicative faults Nonlinear Dynamic Inversion Fault Tolerant Control for Spacecraft    [Volume 8, Issue 2, 2015, Pages 11-17]
N
O
  • Optimal control Optimal Control of a Flexible Spacecraft in a Proximity Operation Using State Dependent Riccati Equation Approach [Volume 8, Issue 1, 2015, Pages 27-41]
  • Optimization algorithm Online Optimal Integrated Guidance and Control Algorithm Design for Launch Vehicle [Volume 8, Issue 2, 2015, Pages 67-78]
  • Optimized environment Solid Fuel Orbiter Designe in Optimized Space Transfer [Volume 8, Issue 1, 2015, Pages 53-60]
  • Orbital element Effect of Time Separation between Observations on Angles-only Preliminary Orbit Determination [Volume 8, Issue 2, 2015, Pages 19-26]
  • Orbital rendezvous and docking Nonlinear Optimal Control of Space Docking and Rendezvous Problem [Volume 8, Issue 3, 2015, Pages 27-40]
  • Orbit Determination Introduction to Tadbir satellite Orbit Determination System [Volume 8, Issue 3, 2015, Pages 65-70]
P
  • Partial stability New Approach in Guidance Law Design Based on Finite-Time Partial Stability Theorem [Volume 8, Issue 1, 2015, Pages 1-7]
  • Piezoelectric layers Active Control of a Smart Satellite under Thermal Loading [Volume 8, Issue 1, 2015, Pages 43-51]
  • Proximity operation Optimal Control of a Flexible Spacecraft in a Proximity Operation Using State Dependent Riccati Equation Approach [Volume 8, Issue 1, 2015, Pages 27-41]
R
  • Radiation Insulations Evaluation of Effective Emissivity of a Multilayer Insulation Blanket Using Test [Volume 8, Issue 1, 2015, Pages 19-25]
  • Re Guidance and Control for Space Capsule in the Presence of Uncertain Dynamic Parameters during the Atmospheric Entry Phase [Volume 8, Issue 3, 2015, Pages 1-13]
  • Reaction wheel Optimal Control of a Tri-axial Spacecraft Simulator Test bed Actuated by Reaction Wheels [Volume 8, Issue 4, 2015, Pages 35-44]
  • Reaction wheels  Design and Implementation of Attitude Control Systemof a satellite with Stereo-Imaging Scenario in Hardware in the Loop Test Bed [Volume 8, Issue 3, 2015, Pages 15-26]
  • Resampling Comparison of Direct and Indirect Georeferencing Methods Using Satellite Linear Array Iimages [Volume 8, Issue 2, 2015, Pages 1-10]
  • Robust Control Design a μ-Controller ToControl Attitude of a Flexible Microsatellite [Volume 8, Issue 1, 2015, Pages 61-71]
S
  • Satellite attitude control Design a μ-Controller ToControl Attitude of a Flexible Microsatellite [Volume 8, Issue 1, 2015, Pages 61-71]
  • Satellite prediction New Satellite Automatic Tracking by Doppler [Volume 8, Issue 2, 2015, Pages 57-65]
  • Separated guidance and control Online Optimal Integrated Guidance and Control Algorithm Design for Launch Vehicle [Volume 8, Issue 2, 2015, Pages 67-78]
  • SGP4 Algorithm Introduction to Tadbir satellite Orbit Determination System [Volume 8, Issue 3, 2015, Pages 65-70]
  • Simulated Annealing Combining Gradient and Evolutionary Algorithms for Improving Collaborative Optimization Performance [Volume 8, Issue 2, 2015, Pages 27-39]
  • Simulation Complementary Method the Conceptual Design of Space Craft Electrical Power  Subsystem [Volume 8, Issue 3, 2015, Pages 55-63]
  • Singularity Design and Manufacturing of a Variable Speed Control Moment Gyro for an Agile Micro-Satellite Attitude Control Simulator [Volume 8, Issue 1, 2015, Pages 73-77]
  • Sliding mode control A New Backstepping Sliding Mode Guidance Law Considering Control Loop Dynamics [Volume 8, Issue 4, 2015, Pages 9-17]
  • Solar panel Complementary Method the Conceptual Design of Space Craft Electrical Power  Subsystem [Volume 8, Issue 3, 2015, Pages 55-63]
  • Spaceborne GPS Receiver Introduction to Tadbir satellite Orbit Determination System [Volume 8, Issue 3, 2015, Pages 65-70]
  • Spacecraft Optimal Control of a Flexible Spacecraft in a Proximity Operation Using State Dependent Riccati Equation Approach [Volume 8, Issue 1, 2015, Pages 27-41]
  • Spacecraft electrical power subsystem Complementary Method the Conceptual Design of Space Craft Electrical Power  Subsystem [Volume 8, Issue 3, 2015, Pages 55-63]
  • State dependent riccati equation Optimal Control of a Flexible Spacecraft in a Proximity Operation Using State Dependent Riccati Equation Approach [Volume 8, Issue 1, 2015, Pages 27-41]
  • State dependent riccati equation Nonlinear Optimal Control of Space Docking and Rendezvous Problem [Volume 8, Issue 3, 2015, Pages 27-40]
  • Stereo Design and Implementation of Attitude Control Systemof a satellite with Stereo-Imaging Scenario in Hardware in the Loop Test Bed [Volume 8, Issue 3, 2015, Pages 15-26]
  • Support Vector Machine Improving DGPS Accuracy Using Predictions of Reference Position Components Error Factors [Volume 8, Issue 2, 2015, Pages 41-56]
T
  • Tadbir Satellite Introduction to Tadbir satellite Orbit Determination System [Volume 8, Issue 3, 2015, Pages 65-70]
  • Terminal conditions Online Optimal Integrated Guidance and Control Algorithm Design for Launch Vehicle [Volume 8, Issue 2, 2015, Pages 67-78]
  • Terminal sliding mode Dynamic Terminal Sliding Mode Control for an Aerospace Launch Vehicle [Volume 8, Issue 4, 2015, Pages 1-7]
  • Thermal loading Active Control of a Smart Satellite under Thermal Loading [Volume 8, Issue 1, 2015, Pages 43-51]
  • Thermal radiation Evaluation of Effective Emissivity of a Multilayer Insulation Blanket Using Test [Volume 8, Issue 1, 2015, Pages 19-25]
  • TLE New Satellite Automatic Tracking by Doppler [Volume 8, Issue 2, 2015, Pages 57-65]
U
  • Uncertainty Optimal Control of a Flexible Spacecraft in a Proximity Operation Using State Dependent Riccati Equation Approach [Volume 8, Issue 1, 2015, Pages 27-41]
  • Uncertainty Design a μ-Controller ToControl Attitude of a Flexible Microsatellite [Volume 8, Issue 1, 2015, Pages 61-71]
  • Unmatched disturbance Dynamic Terminal Sliding Mode Control for an Aerospace Launch Vehicle [Volume 8, Issue 4, 2015, Pages 1-7]
V
  • Variable speed control moment gyro Design and Manufacturing of a Variable Speed Control Moment Gyro for an Agile Micro-Satellite Attitude Control Simulator [Volume 8, Issue 1, 2015, Pages 73-77]
W
  • Wall temperature Aerodynamic Heating Prediction of Flying Body Using Fluid-Solid Conjugate Heat Transfer [Volume 8, Issue 3, 2015, Pages 41-53]
Z
  • ZUPT INS Alignment Improvement Using Rest Heading and Zero-Velocity Updates [Volume 8, Issue 4, 2015, Pages 45-51]