Meysam Mahooti
Available for projects in satellite orbit determination, astrodynamics, and astronomy. If you need my paid source code (https://www.researchgate.net/profile/Meysam-Mahooti/research), please donate in euros using the link below, then email mahooti007@gmail.com with your request. https://pay.ypaylink.com/personal-link/1322/5b99ef3b116d9f19b2442372c97af2bc059f9ed2
MATLAB, Python, C++, C, Java
Spoken Languages:
English
Professional Interests:
Numerical Integration and Differential Equations, Least Squares, Aerospace and Defense, Flight Dynamics, Satellite and Orbital Mechanics
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Feeds
Inviato
Kinematic Orbit Determination
Kinematic Orbit Determination (KOD) for the Swarm-A LEO satellite
circa un mese fa | 28 download |
Inviato
Reduced-Dynamic Orbit Determination
Reduced-Dynamic Orbit Determination for LEO satellites that carry a dual-frequency GPS receiver
circa un mese fa | 39 download |
Inviato
GPS Toolbox
Toolbox for static GPS positioning using RINEX/SP3 data and single-station or double-difference workflows
circa un mese fa | 40 download |
Inviato
ECI2ECEF & ECEF2ECI Transformations
The transformation from celestial to terrestrial reference system and vice versa
circa 2 mesi fa | 2012 download |
Inviato
Real-Time Orbit Determination
Real-Time Orbit Determination based on GPS Navigation Data
2 mesi fa | 1110 download |
Inviato
High Precision Orbit Propagator
Precise modeling of satellite's perturbed motion (special perturbations approach)
2 mesi fa | 8327 download |
Inviato
Satellite Orbit Modeling
Precise modeling of a satellite's perturbed motion (special perturbations approach)
2 mesi fa | 4925 download |
Inviato
Relay Satellite Orbit Determination
Orbit Determination from Tracking and Data Relay Satellite Measurements
2 mesi fa | 1460 download |
Inviato
LEO Launch Window & COLA Screening Tool
daily Low Earth Orbit (LEO) launch opportunities from a geographic launch site into a target orbital plane
3 mesi fa | 25 download |
Inviato
Shampine-Gordon Integrator
Shampine-Gordon is a variable-step, variable-order multi-step integrator.
5 mesi fa | 155 download |
Inviato
Adams-Bashforth-Moulton
Adams-Bashforth-Moulton 8th Order Integration
5 mesi fa | 1321 download |
Inviato
Runge-Kutta-Fehlberg (RKF78)
Adaptive Runge-Kutta-Fehlberg 7(8) Integration
5 mesi fa | 1062 download |
Inviato
Runge-Kutta-Fehlberg (RKF45)
Adaptive Runge-Kutta-Fehlberg 4(5) Integration
5 mesi fa | 2182 download |
Inviato
JPL Development Ephemerides
Computation of the position and velocity of the major planets, the Moon, and the Sun
8 mesi fa | 99 download |
Inviato
Satellite Orbits: Models, Methods and Applications
Satellite Orbits: Models, Methods and Applications
oltre un anno fa | 7046 download |
Inviato
Initial Orbit Determination (Angles-Only Method)
Angles-only approach applying the Least Squares method
oltre un anno fa | 1165 download |
Inviato
Initial Orbit Determination (Extended Kalman Filter)
Initial orbit determination applying the Extended Kalman Filter
oltre un anno fa | 1948 download |
Inviato
Initial Orbit Determination (Least Squares Method)
Initial orbit determination applying the Least Squares method
oltre un anno fa | 1761 download |
Inviato
Moon Phases
Determination of lunar phases and checking for eclipses
oltre un anno fa | 171 download |
Inviato
Local Circumstances of a Solar Eclipse
Computation of possibility of observing solar eclipse at the observer's location
oltre un anno fa | 373 download |
Inviato
Solar Eclipse
Prediction of solar eclipse and its duration using the time of new moon
oltre un anno fa | 891 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
quasi 2 anni fa | 457 download |
Inviato
Jacchia-Bowman Atmospheric Density Model
Computation of the total mass density of the atmosphere using the Jacchia-Bowman model
quasi 2 anni fa | 1720 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).
quasi 2 anni fa | 1344 download |
Inviato
NRLMSISE-00 Atmosphere Model
Computation of neutral temperature and densities in Earth's atmosphere from ground to thermospheric heights.
quasi 2 anni fa | 3411 download |
Inviato
SGP8
The SGP8 model to calculate orbital state vectors of near-Earth satellites
circa 2 anni fa | 607 download |
Inviato
Sun Position (VSOP87)
VSOP87 defines the analytical solutions to the motions of the solar system planets
circa 2 anni fa | 283 download |
Inviato
Moon Position
Position of the Moon referred to the mean equator and equinox of J2000
circa 2 anni fa | 1412 download |









