Meysam Mahooti
University of Tehran
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
NRLMSISE-00 Atmosphere Model
Computation of neutral temperature and densities in Earth's atmosphere from ground to thermospheric heights.
circa 19 ore fa | 51 download |
Inviato
Real-Time Orbit Determination
Real-Time Orbit Determination based on GPS Navigation Data
3 mesi fa | 19 download |
Inviato
SGP8
The SGP8 model to calculate orbital state vectors of near-Earth satellites
3 mesi fa | 15 download |
Inviato
Sun Position (VSOP87)
VSOP87 defines the analytical solutions to the motions of the solar system planets
3 mesi fa | 5 download |
Inviato
Moon Position
Position of the Moon referred to the mean equator and equinox of J2000
3 mesi fa | 8 download |
Inviato
ECI2ECEF & ECEF2ECI Transformations
The transformation from celestial to terrestrial reference system and vice versa
3 mesi fa | 22 download |
Inviato
Sun Position
Geocentric equatorial position of the Sun (in [m]), referred to the ICRF
3 mesi fa | 17 download |
Inviato
Relay Satellite Orbit Determination
Orbit Determination from Tracking and Data Relay Satellite Measurements
5 mesi fa | 7 download |
Inviato
Radau IIA
Variable-order Radau IIA integrator with step-size control
6 mesi fa | 6 download |
Inviato
Satellite Orbit Modeling
Modeling of satellite's perturbed motion (special perturbations approach)
6 mesi fa | 33 download |
Inviato
High Precision Orbit Propagator
Precise modeling of satellite's perturbed motion (special perturbations approach)
6 mesi fa | 74 download |
Inviato
Satellite Visibility
Propagation of the satellite's state vector using SGP4 and checking its visibility for future
7 mesi fa | 5 download |
Inviato
NASA JPL Development Ephemerides (DE405)
DE405 covers 1599-12-09 to 2201-02-20. Referred to the International Celestial Reference Frame.
7 mesi fa | 6 download |
Inviato
Initial orbit determination
Initial orbit determination (two sets of range and angle measurements of a satellite)
8 mesi fa | 4 download |
Inviato
Initial Orbit Determination (Least Squares Method)
Initial orbit determination applying the Least Squares method
9 mesi fa | 14 download |
Inviato
Initial Orbit Determination (Angles-Only Method)
Angles-only approach applying the Least Squares method
9 mesi fa | 12 download |
Inviato
NASA JPL Development Ephemerides (DE440)
High precision planetary ephemerides
10 mesi fa | 5 download |
Inviato
NASA JPL Development Ephemerides (DE441)
High-precision computation of planetary ephemerides
11 mesi fa | 13 download |
Inviato
Lambert's Problem
Lambert’s problem is the orbital boundary-value problem constrained by two points and elapsed time.
12 mesi fa | 17 download |
Inviato
Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times
circa un anno fa | 3 download |
Inviato
Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times
circa un anno fa | 5 download |
Inviato
Initial Orbit Determination (Extended Kalman Filter)
Initial orbit determination applying the Extended Kalman Filter
circa un anno fa | 16 download |
Inviato
Double-r Initial Orbit Determination
Double-r method is utilized to determine the initial orbit.
circa un anno fa | 2 download |
Inviato
Gauss Initial Orbit Determination
Gauss's method is utilized to determine the initial orbit.
circa un anno fa | 12 download |
Inviato
SGP4
The SGP4 model to calculate orbital state vectors of near-Earth satellites
circa un anno fa | 87 download |
Inviato
Moon Phases
Determination of lunar phases and checking for eclipses
oltre un anno fa | 11 download |
Inviato
JPL Development Ephemerides
Computation of position and velocity of major planets, the Moon, and the Sun
oltre un anno fa | 2 download |
Inviato
Solar Eclipse
Prediction of solar eclipse and its duration using the time of new moon
oltre un anno fa | 2 download |
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