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A B C D E F G H I J K L M N O P Q R S T U V W X Y Z ALL

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]