Abdolahi, Sohayla Aerodynamic Heating Prediction of Flying Body Using Fluid-Solid Conjugate Heat Transfer [Volume 8, Issue 3, 2015, Pages 41-53]
Aghalari, Ali Reza 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]
Akbari, Bhzad Comparison of Direct and Indirect Georeferencing Methods Using Satellite Linear Array Iimages [Volume 8, Issue 2, 2015, Pages 1-10]
Akhlomadi, M. R Nonlinear Optimal Control of Space Docking and Rendezvous Problem [Volume 8, Issue 3, 2015, Pages 27-40]
Alikhani, Ali Reza Optimal Control of a Flexible Spacecraft in a Proximity Operation Using State Dependent Riccati Equation Approach [Volume 8, Issue 1, 2015, Pages 27-41]
Alikhani, Ali Reza 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]
Alikhani, Ali Reza Dynamic Terminal Sliding Mode Control for an Aerospace Launch Vehicle [Volume 8, Issue 4, 2016, Pages 1-7]
Alisadeghi, Hamed Evaluation of Effective Emissivity of a Multilayer Insulation Blanket Using Test [Volume 8, Issue 1, 2015, Pages 19-25]
Arabshahi, Hamid Online Optimal Integrated Guidance and Control Algorithm Design for Launch Vehicle [Volume 8, Issue 2, 2015, Pages 67-78]
Ashtari, Mohammad Hassan Introduction to Tadbir satellite Orbit Determination System [Volume 8, Issue 3, 2015, Pages 65-70]
Azadi, Emad Active Control of a Smart Satellite under Thermal Loading [Volume 8, Issue 1, 2015, Pages 43-51]
Azadi, Mohammad Active Control of a Smart Satellite under Thermal Loading [Volume 8, Issue 1, 2015, Pages 43-51]
B
Barati, Ghodratollah Introduction to Tadbir satellite Orbit Determination System [Volume 8, Issue 3, 2015, Pages 65-70]
Basohbat Novinzadeh, Ali Reza Solid Fuel Orbiter Designe in Optimized Space Transfer [Volume 8, Issue 1, 2015, Pages 53-60]
Bazregarzadeh, Elham New Approach in Guidance Law Design Based on Finite-Time Partial Stability Theorem [Volume 8, Issue 1, 2015, Pages 1-7]
Behnamgol, Vahid A New Backstepping Sliding Mode Guidance Law Considering Control Loop Dynamics [Volume 8, Issue 4, 2016, Pages 9-17]
Behzadi, Milad Numerical Investigation of Laminar Premixed Conical Flame Response to Acoustic Excitation [Volume 8, Issue 1, 2015, Pages 9-18]
Binazadeh, Tahere New Approach in Guidance Law Design Based on Finite-Time Partial Stability Theorem [Volume 8, Issue 1, 2015, Pages 1-7]
Bolandi, Hossean Introduction to Tadbir satellite Orbit Determination System [Volume 8, Issue 3, 2015, Pages 65-70]
Bustan, Daniyal Nonlinear Dynamic Inversion Fault Tolerant Control for Spacecraft   [Volume 8, Issue 2, 2015, Pages 11-17]
D
Dameshghi, Adel Improving DGPS Accuracy Using Predictions of Reference Position Components Error Factors [Volume 8, Issue 2, 2015, Pages 41-56]
Darabi, Hossein Combining Gradient and Evolutionary Algorithms for Improving Collaborative Optimization Performance [Volume 8, Issue 2, 2015, Pages 27-39]
E
Ebrahimi, Mohammad Aerodynamic Heating Prediction of Flying Body Using Fluid-Solid Conjugate Heat Transfer [Volume 8, Issue 3, 2015, Pages 41-53]
Esmaeilzadeh, Majed Introduction to Tadbir satellite Orbit Determination System [Volume 8, Issue 3, 2015, Pages 65-70]
Etemadi, Fskhri Aerodynamic Heating Prediction of Flying Body Using Fluid-Solid Conjugate Heat Transfer [Volume 8, Issue 3, 2015, Pages 41-53]
F
Fani Saberi, Farhd 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]
Farshchi, Mohammad Numerical Investigation of Laminar Premixed Conical Flame Response to Acoustic Excitation [Volume 8, Issue 1, 2015, Pages 9-18]
Fathi, Mehdi INS Alignment Improvement Using Rest Heading and Zero-Velocity Updates [Volume 8, Issue 4, 2016, Pages 45-51]
Fathi, Mohsen Design a μ-Controller ToControl Attitude of a Flexible Microsatellite [Volume 8, Issue 1, 2015, Pages 61-71]
Fazelzadeh, Seyed Ahmad Active Control of a Smart Satellite under Thermal Loading [Volume 8, Issue 1, 2015, Pages 43-51]
G
Ghahramani, Nemat Ollah INS Alignment Improvement Using Rest Heading and Zero-Velocity Updates [Volume 8, Issue 4, 2016, Pages 45-51]
Ghobadi, M. Optimal Control of a Tri-axial Spacecraft Simulator Test bed Actuated by Reaction Wheels [Volume 8, Issue 4, 2016, Pages 35-44]
H
Haghi, H. Optimal Control of a Tri-axial Spacecraft Simulator Test bed Actuated by Reaction Wheels [Volume 8, Issue 4, 2016, Pages 35-44]
Hosseini Sani, Seyed Kamal Nonlinear Dynamic Inversion Fault Tolerant Control for Spacecraft   [Volume 8, Issue 2, 2015, Pages 11-17]
I
Izadipour, Ahmad Comparison of Direct and Indirect Georeferencing Methods Using Satellite Linear Array Iimages [Volume 8, Issue 2, 2015, Pages 1-10]
K
Kalhor, Ahmad 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]
Kamali Moghadam, Ramin Equilibrium Effects on the Hypersonic Laminar Boundary Layer Flow over Axisymmetric Bodies [Volume 8, Issue 4, 2016, Pages 19-27]
Kamarzarrin, Mehrnoosh Improving DGPS Accuracy Using Predictions of Reference Position Components Error Factors [Volume 8, Issue 2, 2015, Pages 41-56]
Karimian, Seyed Mohammad Hossein Evaluation of Effective Emissivity of a Multilayer Insulation Blanket Using Test [Volume 8, Issue 1, 2015, Pages 19-25]
Kasaeian, Seyed Aliakbar Dynamic Terminal Sliding Mode Control for an Aerospace Launch Vehicle [Volume 8, Issue 4, 2016, Pages 1-7]
Kashaninia, Abdol Reza Design a μ-Controller ToControl Attitude of a Flexible Microsatellite [Volume 8, Issue 1, 2015, Pages 61-71]
Kochaki, Jafar Introduction to Tadbir satellite Orbit Determination System [Volume 8, Issue 3, 2015, Pages 65-70]
L
Lashkanpour, Majed Effect of Time Separation between Observations on Angles-only Preliminary Orbit Determination [Volume 8, Issue 2, 2015, Pages 19-26]
M
Maleki, Abolfazl Effect of Time Separation between Observations on Angles-only Preliminary Orbit Determination [Volume 8, Issue 2, 2015, Pages 19-26]
Mirshams, M. Optimal Control of a Tri-axial Spacecraft Simulator Test bed Actuated by Reaction Wheels [Volume 8, Issue 4, 2016, Pages 35-44]
Mirshams, Mehrn Complementary Method the Conceptual Design of Space Craft Electrical Power Subsystem [Volume 8, Issue 3, 2015, Pages 55-63]
Moeini, Esmaiel Evaluation of Effective Emissivity of a Multilayer Insulation Blanket Using Test [Volume 8, Issue 1, 2015, Pages 19-25]
Mohammadi, Ali A New Backstepping Sliding Mode Guidance Law Considering Control Loop Dynamics [Volume 8, Issue 4, 2016, Pages 9-17]
Mohsenipour, Reza Design a μ-Controller ToControl Attitude of a Flexible Microsatellite [Volume 8, Issue 1, 2015, Pages 61-71]
Mortazavi, Mohammad Reza Optimal Control of a Flexible Spacecraft in a Proximity Operation Using State Dependent Riccati Equation Approach [Volume 8, Issue 1, 2015, Pages 27-41]
N
Nasirian, M. New Satellite Automatic Tracking by Doppler [Volume 8, Issue 2, 2015, Pages 57-65]
Nasirian, Mehrzad Design a μ-Controller ToControl Attitude of a Flexible Microsatellite [Volume 8, Issue 1, 2015, Pages 61-71]
Navabi, M. Nonlinear Optimal Control of Space Docking and Rendezvous Problem [Volume 8, Issue 3, 2015, Pages 27-40]
Nosrat Elahi, Mehran Solid Fuel Orbiter Designe in Optimized Space Transfer [Volume 8, Issue 1, 2015, Pages 53-60]
P
Pariz, Naser Nonlinear Dynamic Inversion Fault Tolerant Control for Spacecraft   [Volume 8, Issue 2, 2015, Pages 11-17]
R
Refan, Mohammad Hossein Improving DGPS Accuracy Using Predictions of Reference Position Components Error Factors [Volume 8, Issue 2, 2015, Pages 41-56]
R. Najafi, Hamed Evaluation of Effective Emissivity of a Multilayer Insulation Blanket Using Test [Volume 8, Issue 1, 2015, Pages 19-25]
Roshanian, Jafar Combining Gradient and Evolutionary Algorithms for Improving Collaborative Optimization Performance [Volume 8, Issue 2, 2015, Pages 27-39]
Roshanian, Jafar Online Optimal Integrated Guidance and Control Algorithm Design for Launch Vehicle [Volume 8, Issue 2, 2015, Pages 67-78]
S
Saghari, Asad Complementary Method the Conceptual Design of Space Craft Electrical Power Subsystem [Volume 8, Issue 3, 2015, Pages 55-63]
Salimi, Mohammad Reza Equilibrium Effects on the Hypersonic Laminar Boundary Layer Flow over Axisymmetric Bodies [Volume 8, Issue 4, 2016, Pages 19-27]
Shafiei, Mohammad Hossein New Approach in Guidance Law Design Based on Finite-Time Partial Stability Theorem [Volume 8, Issue 1, 2015, Pages 1-7]
Shamadi, Yosef 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]
Shamim, Farhad 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]
Sharifi, Ali Reza Comparison of Direct and Indirect Georeferencing Methods Using Satellite Linear Array Iimages [Volume 8, Issue 2, 2015, Pages 1-10]
T
Tadayon Mousavi, Samaneh Hot Air Gun Identification by Inverse Heat Transfer [Volume 8, Issue 4, 2016, Pages 29-34]
Taei, Hojat Optimal Control of a Tri-axial Spacecraft Simulator Test bed Actuated by Reaction Wheels [Volume 8, Issue 4, 2016, Pages 35-44]
Tahmasbi, Hossein Effect of Time Separation between Observations on Angles-only Preliminary Orbit Determination [Volume 8, Issue 2, 2015, Pages 19-26]
Tahsini, Amir Mahdi Hot Air Gun Identification by Inverse Heat Transfer [Volume 8, Issue 4, 2016, Pages 29-34]
Torabi, Seyed Hossein Online Optimal Integrated Guidance and Control Algorithm Design for Launch Vehicle [Volume 8, Issue 2, 2015, Pages 67-78]
V
Vahid D., M. A. Optimal Control of a Tri-axial Spacecraft Simulator Test bed Actuated by Reaction Wheels [Volume 8, Issue 4, 2016, Pages 35-44]
Vali, Ahmad Reza A New Backstepping Sliding Mode Guidance Law Considering Control Loop Dynamics [Volume 8, Issue 4, 2016, Pages 9-17]
Y
Yousefzade, Meysam Comparison of Direct and Indirect Georeferencing Methods Using Satellite Linear Array Iimages [Volume 8, Issue 2, 2015, Pages 1-10]
Z
Zabihian, Ehsan Complementary Method the Conceptual Design of Space Craft Electrical Power Subsystem [Volume 8, Issue 3, 2015, Pages 55-63]
Zakeri, Mostafa Solid Fuel Orbiter Designe in Optimized Space Transfer [Volume 8, Issue 1, 2015, Pages 53-60]
Zayghami, Mohammad Sadegh Introduction to Tadbir satellite Orbit Determination System [Volume 8, Issue 3, 2015, Pages 65-70]
