Meysam Mahooti
Available for projects in satellite orbit determination, astrodynamics, and astronomy. Contact: mahooti007@gmail.com.
MATLAB, Python, C++, C
Spoken Languages:
English
Professional Interests:
Numerical Integration and Differential Equations, Least Squares, Aerospace and Defense, Flight Dynamics, Satellite and Orbital Mechanics
Statistics
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Feeds
Submitted
Real-Time Orbit Determination
Real-Time Orbit Determination based on GPS Navigation Data
3 days ago | 1089 downloads |
Submitted
High Precision Orbit Propagator
Precise modeling of satellite's perturbed motion (special perturbations approach)
3 days ago | 8263 downloads |
Submitted
Satellite Orbit Modeling
Precise modeling of a satellite's perturbed motion (special perturbations approach)
3 days ago | 4907 downloads |
Submitted
Relay Satellite Orbit Determination
Orbit Determination from Tracking and Data Relay Satellite Measurements
3 days ago | 1448 downloads |
Submitted
Reduced-Dynamic Orbit Determination
Reduced-Dynamic Orbit Determination for LEO satellites that carry a dual-frequency GPS receiver
15 days ago | 24 downloads |
Submitted
LEO Launch Window & COLA Screening Tool
daily Low Earth Orbit (LEO) launch opportunities from a geographic launch site into a target orbital plane
29 days ago | 17 downloads |
Submitted
Kinematic Orbit Determination
Kinematic Orbit Determination (KOD) for the Swarm-A LEO satellite
1 month ago | 15 downloads |
Submitted
GPS Toolbox
Toolbox for static GPS positioning using RINEX/SP3 data and single-station or double-difference workflows
1 month ago | 26 downloads |
Submitted
Shampine-Gordon Integrator
Shampine-Gordon is a variable-step, variable-order multi-step integrator.
3 months ago | 151 downloads |
Submitted
Adams-Bashforth-Moulton
Adams-Bashforth-Moulton 8th Order Integration
3 months ago | 1315 downloads |
Submitted
Runge-Kutta-Fehlberg (RKF78)
Adaptive Runge-Kutta-Fehlberg 7(8) Integration
3 months ago | 1051 downloads |
Submitted
Runge-Kutta-Fehlberg (RKF45)
Adaptive Runge-Kutta-Fehlberg 4(5) Integration
3 months ago | 2166 downloads |
Submitted
JPL Development Ephemerides
Computation of the position and velocity of the major planets, the Moon, and the Sun
6 months ago | 94 downloads |
Submitted
Satellite Orbits: Models, Methods and Applications
Satellite Orbits: Models, Methods and Applications
1 year ago | 7018 downloads |
Submitted
Initial Orbit Determination (Angles-Only Method)
Angles-only approach applying the Least Squares method
1 year ago | 1154 downloads |
Submitted
Initial Orbit Determination (Extended Kalman Filter)
Initial orbit determination applying the Extended Kalman Filter
1 year ago | 1933 downloads |
Submitted
Initial Orbit Determination (Least Squares Method)
Initial orbit determination applying the Least Squares method
1 year ago | 1749 downloads |
Submitted
Moon Phases
Determination of lunar phases and checking for eclipses
1 year ago | 164 downloads |
Submitted
Local Circumstances of a Solar Eclipse
Computation of possibility of observing solar eclipse at the observer's location
1 year ago | 355 downloads |
Submitted
Solar Eclipse
Prediction of solar eclipse and its duration using the time of new moon
1 year ago | 867 downloads |
Submitted
ECI2ECEF & ECEF2ECI Transformations
The transformation from celestial to terrestrial reference system and vice versa
1 year ago | 1995 downloads |
Submitted
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
1 year ago | 450 downloads |
Submitted
Jacchia-Bowman Atmospheric Density Model
Computation of the total mass density of the atmosphere using the Jacchia-Bowman model
1 year ago | 1703 downloads |
Submitted
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).
2 years ago | 1334 downloads |
Submitted
NRLMSISE-00 Atmosphere Model
Computation of neutral temperature and densities in Earth's atmosphere from ground to thermospheric heights.
2 years ago | 3375 downloads |
Submitted
SGP8
The SGP8 model to calculate orbital state vectors of near-Earth satellites
2 years ago | 603 downloads |
Submitted
Sun Position (VSOP87)
VSOP87 defines the analytical solutions to the motions of the solar system planets
2 years ago | 278 downloads |
Submitted
Moon Position
Position of the Moon referred to the mean equator and equinox of J2000
2 years ago | 1399 downloads |









