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Meysam Mahooti


Attivo dal 2016

Followers: 36   Following: 0

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Available for projects in satellite orbit determination, astrodynamics, and astronomy. Contact: mahooti007@gmail.com.

Programming Languages:
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

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Visto da

Inviato


Reduced-Dynamic Orbit Determination
Reduced-Dynamic Orbit Determination for LEO satellites that carry a dual-frequency GPS receiver

2 giorni fa | 18 download |

0.0 / 5

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Satellite Orbit Modeling
Precise modeling of a satellite's perturbed motion (special perturbations approach)

4 giorni fa | 4899 download |

4.1 / 5
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High Precision Orbit Propagator
Precise modeling of satellite's perturbed motion (special perturbations approach)

6 giorni fa | 8238 download |

4.8 / 5
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Inviato


LEO Launch Window & COLA Screening Tool
daily Low Earth Orbit (LEO) launch opportunities from a geographic launch site into a target orbital plane

16 giorni fa | 12 download |

0.0 / 5

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Kinematic Orbit Determination
Kinematic Orbit Determination (KOD) for the Swarm-A LEO satellite

23 giorni fa | 12 download |

0.0 / 5

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GPS Toolbox
Toolbox for static GPS positioning using RINEX/SP3 data and single-station or double-difference workflows

27 giorni fa | 21 download |

0.0 / 5

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Runge-Kutta-Nystrom
Runge-Kutta-Nystrom Integration

circa 2 mesi fa | 431 download |

5.0 / 5

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Shampine-Gordon Integrator
Shampine-Gordon is a variable-step, variable-order multi-step integrator.

3 mesi fa | 151 download |

0.0 / 5

Inviato


Adams-Bashforth-Moulton
Adams-Bashforth-Moulton 8th Order Integration

3 mesi fa | 1315 download |

4.6 / 5

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Runge-Kutta-Fehlberg (RKF78)
Adaptive Runge-Kutta-Fehlberg 7(8) Integration

3 mesi fa | 1050 download |

4.5 / 5
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Runge-Kutta-Fehlberg (RKF45)
Adaptive Runge-Kutta-Fehlberg 4(5) Integration

3 mesi fa | 2161 download |

5.0 / 5
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SGP4/SDP4
SGP4 and SDP4 orbit propagators

3 mesi fa | 529 download |

0.0 / 5
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Inviato


JPL Development Ephemerides
Computation of the position and velocity of the major planets, the Moon, and the Sun

5 mesi fa | 94 download |

0.0 / 5
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Inviato


Relay Satellite Orbit Determination
Orbit Determination from Tracking and Data Relay Satellite Measurements

circa un anno fa | 1444 download |

5.0 / 5
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Inviato


Real-Time Orbit Determination
Real-Time Orbit Determination based on GPS Navigation Data

circa un anno fa | 1082 download |

4.7 / 5
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Inviato


Satellite Orbits: Models, Methods and Applications
Satellite Orbits: Models, Methods and Applications

circa un anno fa | 7015 download |

5.0 / 5
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Initial Orbit Determination (Angles-Only Method)
Angles-only approach applying the Least Squares method

oltre un anno fa | 1149 download |

4.0 / 5
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Initial Orbit Determination (Extended Kalman Filter)
Initial orbit determination applying the Extended Kalman Filter

oltre un anno fa | 1931 download |

5.0 / 5
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Initial Orbit Determination (Least Squares Method)
Initial orbit determination applying the Least Squares method

oltre un anno fa | 1745 download |

5.0 / 5
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Moon Phases
Determination of lunar phases and checking for eclipses

oltre un anno fa | 162 download |

0.0 / 5
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Local Circumstances of a Solar Eclipse
Computation of possibility of observing solar eclipse at the observer's location

oltre un anno fa | 353 download |

4.8 / 5
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Solar Eclipse
Prediction of solar eclipse and its duration using the time of new moon

oltre un anno fa | 865 download |

5.0 / 5
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Inviato


ECI2ECEF & ECEF2ECI Transformations
The transformation from celestial to terrestrial reference system and vice versa

oltre un anno fa | 1993 download |

5.0 / 5
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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

oltre un anno fa | 449 download |

5.0 / 5
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Jacchia-Bowman Atmospheric Density Model
Computation of the total mass density of the atmosphere using the Jacchia-Bowman model

oltre un anno fa | 1696 download |

5.0 / 5
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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 | 1332 download |

4.9 / 5
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NRLMSISE-00 Atmosphere Model
Computation of neutral temperature and densities in Earth's atmosphere from ground to thermospheric heights.

quasi 2 anni fa | 3364 download |

5.0 / 5
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SGP8
The SGP8 model to calculate orbital state vectors of near-Earth satellites

circa 2 anni fa | 600 download |

5.0 / 5
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Sun Position (VSOP87)
VSOP87 defines the analytical solutions to the motions of the solar system planets

circa 2 anni fa | 277 download |

5.0 / 5

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Moon Position
Position of the Moon referred to the mean equator and equinox of J2000

circa 2 anni fa | 1398 download |

4.9 / 5
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