Meysam Mahooti
University of Tehran
Available for projects in satellite orbit determination, astrodynamics, and astronomy. Contact: mahooti007@gmail.com.
C++, C, MATLAB
Spoken Languages:
English
Professional Interests:
Numerical Integration and Differential Equations, Least Squares, Aerospace and Defense, Flight Dynamics, Satellite and Orbital Mechanics
Feeds
已提交
Relay Satellite Orbit Determination
Orbit Determination from Tracking and Data Relay Satellite Measurements
8 months 前 | 3 次下载 |
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Real-Time Orbit Determination
Real-Time Orbit Determination based on GPS Navigation Data
8 months 前 | 10 次下载 |
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Satellite Orbit Modeling
Precise modeling of satellite's perturbed motion (special perturbations approach)
8 months 前 | 8 次下载 |
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Satellite Orbits: Models, Methods and Applications
Satellite Orbits: Models, Methods and Applications
8 months 前 | 25 次下载 |
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High Precision Orbit Propagator
Precise modeling of satellite's perturbed motion (special perturbations approach)
8 months 前 | 48 次下载 |
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Initial Orbit Determination (Angles-Only Method)
Angles-only approach applying the Least Squares method
11 months 前 | 5 次下载 |
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Initial Orbit Determination (Extended Kalman Filter)
Initial orbit determination applying the Extended Kalman Filter
11 months 前 | 7 次下载 |
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Initial Orbit Determination (Least Squares Method)
Initial orbit determination applying the Least Squares method
11 months 前 | 7 次下载 |
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Local Circumstances of a Solar Eclipse
Computation of possibility of observing solar eclipse at the observer's location
11 months 前 | 1 次下载 |
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Solar Eclipse
Prediction of solar eclipse and its duration using the time of new moon
11 months 前 | 1 次下载 |
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ECI2ECEF & ECEF2ECI Transformations
The transformation from celestial to terrestrial reference system and vice versa
12 months 前 | 8 次下载 |
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Positions of solar system bodies
The heliocentric and geocentric positions of the solar system's eight planets, in addition to the Moon and the Sun
1 year 前 | 3 次下载 |
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Jacchia-Bowman Atmospheric Density Model
Computation of the total mass density of the atmosphere using the Jacchia-Bowman model
1 year 前 | 9 次下载 |
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NASA JPL Development Ephemerides (DE430)
DE430 spans from 1549-12-21 to 2650-01-25 and is based on the International Celestial Reference Frame (version 2.0).
1 year 前 | 8 次下载 |
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NRLMSISE-00 Atmosphere Model
Computation of neutral temperature and densities in Earth's atmosphere from ground to thermospheric heights.
1 year 前 | 30 次下载 |
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SGP8
The SGP8 model to calculate orbital state vectors of near-Earth satellites
1 year 前 | 5 次下载 |
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Sun Position (VSOP87)
VSOP87 defines the analytical solutions to the motions of the solar system planets
1 year 前 | 1 次下载 |
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Moon Position
Position of the Moon referred to the mean equator and equinox of J2000
1 year 前 | 2 次下载 |
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Sun Position
Geocentric equatorial position of the Sun (in [m]), referred to the ICRF
1 year 前 | 16 次下载 |
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Satellite Visibility
Propagation of the satellite's state vector using SGP4 and checking its visibility for future
2 years 前 | 8 次下载 |
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NASA JPL Development Ephemerides (DE405)
DE405 covers 1599-12-09 to 2201-02-20. Referred to the International Celestial Reference Frame.
2 years 前 | 6 次下载 |
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Initial orbit determination
Initial orbit determination (two sets of range and angle measurements of a satellite)
2 years 前 | 5 次下载 |
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NASA JPL Development Ephemerides (DE440)
High precision planetary ephemerides
2 years 前 | 11 次下载 |
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NASA JPL Development Ephemerides (DE441)
High-precision computation of planetary ephemerides
2 years 前 | 6 次下载 |
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Lambert's Problem
Lambert’s problem is the orbital boundary-value problem constrained by two points and elapsed time.
2 years 前 | 3 次下载 |
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Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times
2 years 前 | 1 次下载 |
已提交
Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times
2 years 前 | 4 次下载 |









