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Meysam Mahooti
University of Tehran
I am a consultant for projects related to my file exchange source code. You can reach me at mahooti007@gmail.com.
MATLAB
Spoken Languages:
English
Professional Interests:
Numerical Integration and Differential Equations, Least Squares, Aerospace and Defense, Satellite and Orbital Mechanics
Statistiques
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A soumis
ECI2ECEF & ECEF2ECI Transformations
The transformation from celestial to terrestrial reference system and vice versa
3 jours il y a | 24 téléchargements |
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A soumis
High Precision Orbit Propagator
Precise modeling of satellite's perturbed motion (special perturbations approach)
3 jours il y a | 71 téléchargements |
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A soumis
Real-Time Orbit Determination
Real-Time Orbit Determination based on GPS Navigation Data
4 jours il y a | 14 téléchargements |
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A soumis
Relay Satellite Orbit Determination
Orbit Determination from Tracking and Data Relay Satellite Measurements
4 jours il y a | 10 téléchargements |
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A soumis
Satellite Orbit Modeling
Precise modeling of satellite's perturbed motion (special perturbations approach)
5 jours il y a | 34 téléchargements |
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A soumis
Initial Orbit Determination (Least Squares Method)
Initial orbit determination applying the Least Squares method
environ un mois il y a | 12 téléchargements |
A soumis
Initial Orbit Determination (Extended Kalman Filter)
Initial orbit determination applying the Extended Kalman Filter
environ un mois il y a | 15 téléchargements |
A soumis
Satellite Orbits: Models, Methods and Applications
Satellite Orbits: Models, Methods and Applications
2 mois il y a | 37 téléchargements |
A soumis
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
2 mois il y a | 3 téléchargements |
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A soumis
Jacchia-Bowman Atmospheric Density Model
Computation of the total mass density of the atmosphere using the Jacchia-Bowman model
3 mois il y a | 14 téléchargements |
A soumis
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).
3 mois il y a | 12 téléchargements |
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A soumis
Runge-Kutta-Fehlberg (RKF78)
Fehlberg's 7th and 8th Order Embedded Method
3 mois il y a | 7 téléchargements |
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A soumis
NRLMSISE-00 Atmosphere Model
Computation of neutral temperature and densities in Earth's atmosphere from ground to thermospheric heights.
3 mois il y a | 34 téléchargements |
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A soumis
SGP8
The SGP8 model to calculate orbital state vectors of near-Earth satellites
6 mois il y a | 7 téléchargements |
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A soumis
Sun Position (VSOP87)
VSOP87 defines the analytical solutions to the motions of the solar system planets
6 mois il y a | 3 téléchargements |
A soumis
Moon Position
Position of the Moon referred to the mean equator and equinox of J2000
6 mois il y a | 12 téléchargements |
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A soumis
Sun Position
Geocentric equatorial position of the Sun (in [m]), referred to the ICRF
6 mois il y a | 15 téléchargements |
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A soumis
Radau IIA
Variable-order Radau IIA integrator with step-size control
9 mois il y a | 2 téléchargements |
A soumis
Satellite Visibility
Propagation of the satellite's state vector using SGP4 and checking its visibility for future
10 mois il y a | 8 téléchargements |
A soumis
NASA JPL Development Ephemerides (DE405)
DE405 covers 1599-12-09 to 2201-02-20. Referred to the International Celestial Reference Frame.
11 mois il y a | 12 téléchargements |
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A soumis
Initial orbit determination
Initial orbit determination (two sets of range and angle measurements of a satellite)
11 mois il y a | 2 téléchargements |
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A soumis
Initial Orbit Determination (Angles-Only Method)
Angles-only approach applying the Least Squares method
12 mois il y a | 10 téléchargements |
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A soumis
NASA JPL Development Ephemerides (DE440)
High precision planetary ephemerides
environ un an il y a | 6 téléchargements |
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A soumis
NASA JPL Development Ephemerides (DE441)
High-precision computation of planetary ephemerides
environ un an il y a | 11 téléchargements |
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A soumis
Lambert's Problem
Lambert’s problem is the orbital boundary-value problem constrained by two points and elapsed time.
environ un an il y a | 11 téléchargements |
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A soumis
Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times
plus d'un an il y a | 2 téléchargements |
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A soumis
Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times
plus d'un an il y a | 1 téléchargement |
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A soumis
Double-r Initial Orbit Determination
Double-r method is utilized to determine the initial orbit.
plus d'un an il y a | 7 téléchargements |
A soumis
Gauss Initial Orbit Determination
Gauss's method is utilized to determine the initial orbit.
plus d'un an il y a | 9 téléchargements |