Meysam Mahooti
University of Tehran
I accept projects related to satellite orbit determination and astronomy. You can reach me at mahooti007@gmail.com.
C++, C, MATLAB
Spoken Languages:
English
Professional Interests:
Numerical Integration and Differential Equations, Least Squares, Aerospace and Defense, Satellite and Orbital Mechanics
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Feeds
Inviato
Relay Satellite Orbit Determination
Orbit Determination from Tracking and Data Relay Satellite Measurements
6 mesi fa | 5 download |
Inviato
Real-Time Orbit Determination
Real-Time Orbit Determination based on GPS Navigation Data
6 mesi fa | 13 download |
Inviato
Satellite Orbit Modeling
Precise modeling of satellite's perturbed motion (special perturbations approach)
6 mesi fa | 7 download |
Inviato
Satellite Orbits: Models, Methods and Applications
Satellite Orbits: Models, Methods and Applications
6 mesi fa | 25 download |
Inviato
High Precision Orbit Propagator
Precise modeling of satellite's perturbed motion (special perturbations approach)
6 mesi fa | 40 download |
Inviato
Initial Orbit Determination (Angles-Only Method)
Angles-only approach applying the Least Squares method
10 mesi fa | 6 download |
Inviato
Initial Orbit Determination (Extended Kalman Filter)
Initial orbit determination applying the Extended Kalman Filter
10 mesi fa | 8 download |
Inviato
Initial Orbit Determination (Least Squares Method)
Initial orbit determination applying the Least Squares method
10 mesi fa | 10 download |
Inviato
Moon Phases
Determination of lunar phases and checking for eclipses
10 mesi fa | 4 download |
Inviato
Local Circumstances of a Solar Eclipse
Computation of possibility of observing solar eclipse at the observer's location
10 mesi fa | 1 download |
Inviato
Solar Eclipse
Prediction of solar eclipse and its duration using the time of new moon
10 mesi fa | 2 download |
Inviato
ECI2ECEF & ECEF2ECI Transformations
The transformation from celestial to terrestrial reference system and vice versa
10 mesi fa | 9 download |
Inviato
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
circa un anno fa | 3 download |
Inviato
Jacchia-Bowman Atmospheric Density Model
Computation of the total mass density of the atmosphere using the Jacchia-Bowman model
circa un anno fa | 10 download |
Inviato
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).
circa un anno fa | 10 download |
Inviato
Runge-Kutta-Fehlberg (RKF78)
Fehlberg's 7th and 8th Order Embedded Method
circa un anno fa | 3 download |
Inviato
NRLMSISE-00 Atmosphere Model
Computation of neutral temperature and densities in Earth's atmosphere from ground to thermospheric heights.
circa un anno fa | 38 download |
Inviato
SGP8
The SGP8 model to calculate orbital state vectors of near-Earth satellites
oltre un anno fa | 8 download |
Inviato
Sun Position (VSOP87)
VSOP87 defines the analytical solutions to the motions of the solar system planets
oltre un anno fa | 3 download |
Inviato
Moon Position
Position of the Moon referred to the mean equator and equinox of J2000
oltre un anno fa | 6 download |
Inviato
Sun Position
Geocentric equatorial position of the Sun (in [m]), referred to the ICRF
oltre un anno fa | 9 download |
Inviato
Radau IIA
Variable-order Radau IIA integrator with step-size control
oltre un anno fa | 5 download |
Inviato
Satellite Visibility
Propagation of the satellite's state vector using SGP4 and checking its visibility for future
oltre un anno fa | 6 download |
Inviato
NASA JPL Development Ephemerides (DE405)
DE405 covers 1599-12-09 to 2201-02-20. Referred to the International Celestial Reference Frame.
oltre un anno fa | 5 download |
Inviato
Initial orbit determination
Initial orbit determination (two sets of range and angle measurements of a satellite)
oltre un anno fa | 5 download |
Inviato
NASA JPL Development Ephemerides (DE440)
High precision planetary ephemerides
quasi 2 anni fa | 7 download |
Inviato
NASA JPL Development Ephemerides (DE441)
High-precision computation of planetary ephemerides
quasi 2 anni fa | 13 download |
Inviato
Lambert's Problem
Lambert’s problem is the orbital boundary-value problem constrained by two points and elapsed time.
circa 2 anni fa | 15 download |
Inviato
Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times
oltre 2 anni fa | 6 download |
Inviato
Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times
oltre 2 anni fa | 4 download |
