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

  • 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

  • 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]