Meysam Mahooti
University of Tehran
MATLAB
Spoken Languages:
English
Professional Interests:
Numerical Integration and Differential Equations, Aerospace, Satellite and Orbital Mechanics
Statistics
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Download any 10 unique submissions
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Feeds
Submitted
Real-Time Orbit Determination
Real-Time Orbit Determination based on GPS Navigation Data
7 hours ago | 11 downloads |
Submitted
SGP8
The SGP8 model to calculate orbital state vectors of near-Earth satellites
2 days ago | 12 downloads |
Submitted
Sun Position (VSOP87)
VSOP87 defines the analytical solutions to the motions of the solar system planets
2 days ago | 5 downloads |
Submitted
Moon Position
Position of the Moon referred to the mean equator and equinox of J2000
3 days ago | 13 downloads |
Submitted
ECI2ECEF & ECEF2ECI Transformations
The transformation from celestial to terrestrial reference system and vice versa
4 days ago | 41 downloads |
Submitted
Sun Position
Geocentric equatorial position of the Sun (in [m]), referred to the ICRF
11 days ago | 26 downloads |
Submitted
ELFIND
ELFIND approximates an unknown orbit from two or three observations.
12 days ago | 2 downloads |
Submitted
Relay Satellite Orbit Determination
Orbit Determination from Tracking and Data Relay Satellite Measurements
3 months ago | 11 downloads |
Submitted
Radau IIA
Variable-order Radau IIA integrator with step-size control
3 months ago | 2 downloads |
Submitted
Satellite Orbit Modeling
Modeling of satellite's perturbed motion (special perturbations approach)
3 months ago | 27 downloads |
Submitted
High Precision Orbit Propagator
Precise modeling of satellite's perturbed motion (special perturbations approach)
3 months ago | 54 downloads |
Submitted
Satellite Visibility
Propagation of the satellite's state vector using SGP4 and checking its visibility for future
4 months ago | 11 downloads |
Submitted
NASA JPL Development Ephemerides (DE405)
DE405 covers 1599-12-09 to 2201-02-20. Referred to the International Celestial Reference Frame.
5 months ago | 8 downloads |
Submitted
Initial orbit determination
Initial orbit determination (two sets of range and angle measurements of a satellite)
5 months ago | 7 downloads |
Submitted
Initial Orbit Determination (Least Squares Method)
Initial orbit determination applying the Least Squares method
6 months ago | 19 downloads |
Submitted
Initial Orbit Determination (Angles-Only Method)
Angles-only approach applying the Least Squares method
6 months ago | 14 downloads |
Submitted
NASA JPL Development Ephemerides (DE440)
High precision planetary ephemerides
7 months ago | 5 downloads |
Submitted
NASA JPL Development Ephemerides (DE441)
High-precision computation of planetary ephemerides
8 months ago | 11 downloads |
Submitted
Lambert's Problem
Lambert’s problem is the orbital boundary-value problem constrained by two points and elapsed time.
9 months ago | 8 downloads |
Submitted
Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times
11 months ago | 2 downloads |
Submitted
Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times
11 months ago | 2 downloads |
Submitted
Initial Orbit Determination (Extended Kalman Filter)
Initial orbit determination applying the Extended Kalman Filter
12 months ago | 17 downloads |
Submitted
Double-r Initial Orbit Determination
Double-r method is utilized to determine the initial orbit.
12 months ago | 3 downloads |
Submitted
Gauss Initial Orbit Determination
Gauss's method is utilized to determine the initial orbit.
12 months ago | 7 downloads |
Submitted
SGP4
The SGP4 model to calculate orbital state vectors of near-Earth satellites
12 months ago | 77 downloads |
Submitted
Moon Phases
Determination of lunar phases and checking for eclipses
1 year ago | 2 downloads |
Submitted
JPL Development Ephemerides
Computation of position and velocity of major planets, the Moon, and the Sun
1 year ago | 3 downloads |
Submitted
Solar Eclipse
Prediction of solar eclipse and its duration using the time of new moon
1 year ago | 2 downloads |
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