Meysam Mahooti

University of Tehran

Attivo dal 2016

Followers: 20 Following: 0

Messaggio

I am a consultant for projects related to my file exchange source code. You can reach me at mahooti007@gmail.com.

Programming Languages:
MATLAB
Spoken Languages:
English
Professional Interests:
Numerical Integration and Differential Equations, Least Squares, Aerospace and Defense, Satellite and Orbital Mechanics

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Inviato

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

8 giorni fa | 10 download |

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

9 giorni fa | 17 download |

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

circa un mese fa | 38 download |

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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

circa un mese fa | 7 download |

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

circa 2 mesi fa | 17 download |

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

circa 2 mesi fa | 78 download |

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

circa 2 mesi fa | 25 download |

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

circa 2 mesi fa | 9 download |

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

circa 2 mesi fa | 13 download |

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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 mesi fa | 9 download |

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Runge-Kutta-Fehlberg (RKF78)
Fehlberg's 7th and 8th Order Embedded Method

2 mesi fa | 12 download |

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

2 mesi fa | 35 download |

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

5 mesi fa | 6 download |

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

5 mesi fa | 4 download |

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

5 mesi fa | 10 download |

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

5 mesi fa | 21 download |

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Sun Position
Geocentric equatorial position of the Sun (in [m]), referred to the ICRF

5 mesi fa | 7 download |

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Radau IIA
Variable-order Radau IIA integrator with step-size control

8 mesi fa | 4 download |

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Satellite Visibility
Propagation of the satellite's state vector using SGP4 and checking its visibility for future

9 mesi fa | 6 download |

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NASA JPL Development Ephemerides (DE405)
DE405 covers 1599-12-09 to 2201-02-20. Referred to the International Celestial Reference Frame.

10 mesi fa | 6 download |

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Initial orbit determination
Initial orbit determination (two sets of range and angle measurements of a satellite)

10 mesi fa | 3 download |

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

11 mesi fa | 7 download |

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NASA JPL Development Ephemerides (DE440)
High precision planetary ephemerides

12 mesi fa | 9 download |

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NASA JPL Development Ephemerides (DE441)
High-precision computation of planetary ephemerides

circa un anno fa | 10 download |

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Lambert's Problem
Lambert’s problem is the orbital boundary-value problem constrained by two points and elapsed time.

circa un anno fa | 13 download |

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Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times

oltre un anno fa | 2 download |

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Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times

oltre un anno fa | 1 download |

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Double-r Initial Orbit Determination
Double-r method is utilized to determine the initial orbit.

oltre un anno fa | 5 download |

Inviato

Gauss Initial Orbit Determination
Gauss's method is utilized to determine the initial orbit.

oltre un anno fa | 9 download |

Inviato

SGP4/SDP4
SGP4 and SDP4 orbit propagators

oltre un anno fa | 13 download |

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Meysam Mahooti

University of Tehran

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File Exchange

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File Exchange

File Exchange

File Exchange

File Exchange

File Exchange

MATLAB Answers

MATLAB Answers

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