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Astronomy
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keywords:("Astronomy")
DEGRADATION OF THE REFLECTANCE PROPERTIES OF SOME GSS IN SPACE, PRELIMINARY RESULTS
Use of satellite navigation systems for transport monitoring
Relationship between chemical and mineralogical parameters of Moon surface and color-index
Forming optimal routes in the problems of transport logistics by use of GIS technology
Investigation of MEMS IMU Performance in Sounding Rocket
States' Responsibility to Operate Small Satellites in International Space Law
Using of GIS technology in problems of transport logistics
Investigation of Length and Velocity Variation Effects on Unsteady Separation of Parallel Boosters
Dynamic Simulation for Diffusion of Satellite Detached Particles in Various Orbits
Role of States in Regulating Space Activities in International Law
A Survey on Vision Navigation Methods for UAV Navigation Applications
Design and Dynamic Analysis for Vertical and Horizontal Cylindrical Body in Reentry Flight
A Nonlinear Attitude Controller for a Launch Abort System of a Manned Spacecraft
Inertial navigation position error estimation, using vision system
Using navigational technologies in geologistics problems
Passage of Space Objects over the Territory of States from the Perspective of the International Law
Usinge The qEKF Algorithm for Satellite Attitude Estimation with Two Magnetometer & Sun Sensors
Comprehensive Pattern in Designing Low-Thrust Space Propulsion Systems
الگوریتم جدید فرا ابتکاری تطبیقی در تخمین وضعیت و مدل فضاپیما
GPS Signal Simulation in Intermediate Frequency (IF)
Empirical Modeling of Clarity in the Caspian Sea using MERIS Data
System Design and Analysis of Launch Abort System of Manned Spacecraft in Sub-Orbital Mission
Space Inertial Navigation System Accuracy Increasing Using Orbit Point Mass Dynamic
هدایت بهینه بر خط بازگشت به زمین از طریق بسط مجانبی هماهنگ
Investigation and Analysis of Seperation System of Kavoshgar-3
Drivation of System Level Characteristics of a Manned Spacecraft by Applying Statistics Models
The Turbulence Model in the Spacecraft by using A Moving Pulsed Ball Model
Flight Path Angle Steering with Lambert Guidance Reference
Spacecraft Optimal Attitude Control by means of Reaction Wheels
Optimal Control of Low Propulsion Orbital Transfer Time
Attitude nonlinear predictive control of an under actuated spacecraft
Optimum Transition Orbit Design for Launch Vehicles
کاربرد مدل پاندول ساده به منظور اعمال دینامیک تلاطم سیال در شبیهسازی شش درجه آزادی پرواز ماهوارهبر
An Algorithm for Increasing Performance of a Space Launch Vehicle Using Solid Rocket Boosters
Modeling and Control of Fuel Sloshing and its Effect on Spacecraft Attitude
Optimal Mission Design for Moon Exploration Expedition
Considerations of Utilizing Telemetry and GPS System in Sounding Rockets
Effects of Some Parameters on Thermal Control of a LEO Satellite