A
-
Aghalari, A.R.
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]
-
AlizadehYazdi, Mehdi
Experimental Analysis of Pyroshock Wave Propagation in Kavoshgar's Payload [Volume 7, Issue 4, 2015]
-
Anvari, A.
Effects of Some Parameters on Thermal Control of a LEO Satellite [Volume 7, Issue 1, 2014]
B
-
Bahrami, M.
Fuzzy Sliding Mode for Spacecraft Formation Control in Eccentric Orbits [Volume 7, Issue 1, 2014]
-
Bahrami, Mohsen
Verification of a Low Cost Method for Accelerometers Calibration with a Two-Axis Table [Volume 7, Issue 4, 2015]
-
Basohbat Novinzadeh, Ali Reza
Integrated Design of Orbital Transfer Block in an Optimized and Multistep Converged Environment [Volume 7, Issue 4, 2015]
-
Bemani, Vali
Integrated Design of Orbital Transfer Block in an Optimized and Multistep Converged Environment [Volume 7, Issue 4, 2015]
-
Bustan, D.
Intelligent Satellite Orbit Prediction Based on Time Series Analysis [Volume 7, Issue 3, 2014]
C
-
Cheheltani, S. H.
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]
-
Chekini, A.
FPGA Implementation of JPEG and JPEG2000-Based Dynamic Partial Reconfiguration on SOC for Remote Sensing Satellite On-Board Processing [Volume 7, Issue 1, 2014]
D
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Dehghan, S. M. M.
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]
E
-
Ebrahimi, Mohammad
Experimental Analysis of Pyroshock Wave Propagation in Kavoshgar's Payload [Volume 7, Issue 4, 2015]
-
Emadi Noori, Yazdan
Integrated Design of Orbital Transfer Block in an Optimized and Multistep Converged Environment [Volume 7, Issue 4, 2015]
-
Emami, R.
Satellite Conceptual Design Multi-Objective Optimization Using Co Framework [Volume 7, Issue 1, 2014]
-
Eslami, A. A.
Reliability Determination of a Sounding Rocket Separation System Using its Reliability Block Diagram and FMEA [Volume 7, Issue 1, 2014]
F
-
Farajollahi, Hossein
Isolation of Satellite's Sensitive Equipments from Longitudinal Vibration of Launch Vehicle Using Silicone Gel [Volume 7, Issue 4, 2015]
-
Farhani, F.
Effects of Some Parameters on Thermal Control of a LEO Satellite [Volume 7, Issue 1, 2014]
-
Farsi, M. A.
Reliability Determination of a Sounding Rocket Separation System Using its Reliability Block Diagram and FMEA [Volume 7, Issue 1, 2014]
-
Farsi, Mohammad Ali
Experimental Analysis of Pyroshock Wave Propagation in Kavoshgar's Payload [Volume 7, Issue 4, 2015]
-
Faryadi, S.
Remote Sensing Role in Land Use StudiesCase Study: Tehran Metropolitan and its Boundary [Volume 7, Issue 3, 2014]
-
Fazeli, H.
Comprehensive Pattern in Designing Low-Thrust Space Propulsion Systems [Volume 7, Issue 3, 2014]
G
-
Ghasemloo, S.
Approximate Viscous Shock-Layer Analysis of Axisymmetric Bodies in Perfect Gas Hypersonic Flow [Volume 7, Issue 1, 2014]
-
Gheisari, M.M.
Second Order Level Set Method in Numerical Simulation of the Grain Burn-Back [Volume 7, Issue 3, 2014]
-
Gorgin, R.
Reliability Determination of a Sounding Rocket Separation System Using its Reliability Block Diagram and FMEA [Volume 7, Issue 1, 2014]
H
-
Hosseini, S. A.
Laminar and Turbulent Aero Heating Predictions over Blunt Body in Hypersonic Flow [Volume 7, Issue 1, 2014]
-
HosseiniSani, S. K.
Intelligent Satellite Orbit Prediction Based on Time Series Analysis [Volume 7, Issue 3, 2014]
I
-
Imani, A.
Fuzzy Sliding Mode for Spacecraft Formation Control in Eccentric Orbits [Volume 7, Issue 1, 2014]
J
-
Jafarsalehi, A.
Satellite Conceptual Design Multi-Objective Optimization Using Co Framework [Volume 7, Issue 1, 2014]
-
Jahani, Kamal
Isolation of Satellite's Sensitive Equipments from Longitudinal Vibration of Launch Vehicle Using Silicone Gel [Volume 7, Issue 4, 2015]
-
Jalali Naini, Seyed Hamid
Implicit Guidance Equations in Polar Coordinates [Volume 7, Issue 4, 2015]
-
Jalali-Naini, S. H.
Ascending Phase Fuzzy Logic Guidance of Satellite Launch Vehicles for Reducing the Adverse Wind Effects [Volume 7, Issue 3, 2014]
K
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Kalhor, A.
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]
-
Kazemi, H.
Passage of Space Objects over the Territory of States from the Perspective of the International Law [Volume 7, Issue 3, 2014]
M
-
Makhdoum, M. F.
Remote Sensing Role in Land Use StudiesCase Study: Tehran Metropolitan and its Boundary [Volume 7, Issue 3, 2014]
-
Mirsajedi, S. M.
Second Order Level Set Method in Numerical Simulation of the Grain Burn-Back [Volume 7, Issue 3, 2014]
-
Mirshams, M.
Satellite Conceptual Design Multi-Objective Optimization Using Co Framework [Volume 7, Issue 1, 2014]
-
Mirshams, M.
Comprehensive Pattern in Designing Low-Thrust Space Propulsion Systems [Volume 7, Issue 3, 2014]
-
Mirzaei, Hamid Reza
Attitude Control of Spacecraft by State Dependent Riccati Equation and Power Series Expansion of Riccati Methods [Volume 7, Issue 4, 2015]
-
Mirza Kuchaki, Satar
Precise Positioning in GPS Receivers for Very High Velocities Using Combination of Recursive Least Squares and Fuzzy Logic [Volume 7, Issue 4, 2015]
-
Mortazavi, Seyed Hossein
Analytical Solution to Relative Motion Dynamics in Satellite Formation Flying Using Geostationary Orbit Sets [Volume 7, Issue 4, 2015]
-
Mosavi, Seyed Mohammad Reza
Precise Positioning in GPS Receivers for Very High Velocities Using Combination of Recursive Least Squares and Fuzzy Logic [Volume 7, Issue 4, 2015]
N
-
Naji, H. R.
FPGA Implementation of JPEG and JPEG2000-Based Dynamic Partial Reconfiguration on SOC for Remote Sensing Satellite On-Board Processing [Volume 7, Issue 1, 2014]
-
Naseh, H.
Comprehensive Pattern in Designing Low-Thrust Space Propulsion Systems [Volume 7, Issue 3, 2014]
-
Navabi, Mohammad
Attitude Control of Spacecraft by State Dependent Riccati Equation and Power Series Expansion of Riccati Methods [Volume 7, Issue 4, 2015]
-
Nikkhah, A. A.
Extracting the Non-ObservableStates in Alignment & Calibration Process for Gimballed Inertial Navigation Systems [Volume 7, Issue 3, 2014]
-
Nobahari, H.
Extracting the Non-ObservableStates in Alignment & Calibration Process for Gimballed Inertial Navigation Systems [Volume 7, Issue 3, 2014]
-
Noori, S.
Laminar and Turbulent Aero Heating Predictions over Blunt Body in Hypersonic Flow [Volume 7, Issue 1, 2014]
-
Noori, S.
Approximate Viscous Shock-Layer Analysis of Axisymmetric Bodies in Perfect Gas Hypersonic Flow [Volume 7, Issue 1, 2014]
-
Nosrat Elahi, Mehran
Integrated Design of Orbital Transfer Block in an Optimized and Multistep Converged Environment [Volume 7, Issue 4, 2015]
-
Novinzadeh, A.B.
Comprehensive Pattern in Designing Low-Thrust Space Propulsion Systems [Volume 7, Issue 3, 2014]
P
-
Pariz, N.
Intelligent Satellite Orbit Prediction Based on Time Series Analysis [Volume 7, Issue 3, 2014]
-
Parsi, Behzad
Verification of a Low Cost Method for Accelerometers Calibration with a Two-Axis Table [Volume 7, Issue 4, 2015]
R
-
Rahemi, Narjes
Precise Positioning in GPS Receivers for Very High Velocities Using Combination of Recursive Least Squares and Fuzzy Logic [Volume 7, Issue 4, 2015]
S
-
SalehiAmiri, S. M.
Extracting the Non-ObservableStates in Alignment & Calibration Process for Gimballed Inertial Navigation Systems [Volume 7, Issue 3, 2014]
-
Sayahnia, R.
Remote Sensing Role in Land Use StudiesCase Study: Tehran Metropolitan and its Boundary [Volume 7, Issue 3, 2014]
-
Sohrab, M.
Ascending Phase Fuzzy Logic Guidance of Satellite Launch Vehicles for Reducing the Adverse Wind Effects [Volume 7, Issue 3, 2014]
T
-
Tahaye Abadi, Mohammad
Experimental Analysis of Pyroshock Wave Propagation in Kavoshgar's Payload [Volume 7, Issue 4, 2015]
-
Tavana, Mina
Attitude Control of Spacecraft by State Dependent Riccati Equation and Power Series Expansion of Riccati Methods [Volume 7, Issue 4, 2015]
Z
-
Zakeri, Mostafa
Integrated Design of Orbital Transfer Block in an Optimized and Multistep Converged Environment [Volume 7, Issue 4, 2015]
-
Zardashti, R.
Ascending Phase Fuzzy Logic Guidance of Satellite Launch Vehicles for Reducing the Adverse Wind Effects [Volume 7, Issue 3, 2014]