Meysam Mahooti

Attivo dal 2016

Followers: 31 Following: 0

Messaggio

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

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

Statistica

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Inviato

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

circa 15 ore fa | 6 download |

0.0 / 5

Inviato

LEO Launch Window Calculator
LEO Launch Window Calculator with COLA (Collision on Launch Avoidance)

3 giorni fa | 3 download |

0.0 / 5

Inviato

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

4 giorni fa | 11 download |

0.0 / 5

Inviato

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

5 giorni fa | 5 download |

0.0 / 5

Inviato

Runge-Kutta-Nystrom
Runge-Kutta-Nystrom Integration

29 giorni fa | 5 download |

5.0 / 5

Inviato

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

circa 2 mesi fa | 5 download |

0.0 / 5

Inviato

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

circa 2 mesi fa | 3 download |

4.6 / 5

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

circa 2 mesi fa | 3 download |

4.5 / 5

Inviato

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

circa 2 mesi fa | 5 download |

5.0 / 5

Inviato

SGP4/SDP4
SGP4 and SDP4 orbit propagators

2 mesi fa | 11 download |

0.0 / 5

Inviato

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

5 mesi fa | 3 download |

0.0 / 5

Inviato

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

circa un anno fa | 2 download |

5.0 / 5

Inviato

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

circa un anno fa | 4 download |

4.7 / 5

Inviato

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

circa un anno fa | 7 download |

4.1 / 5

Inviato

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

circa un anno fa | 11 download |

5.0 / 5

Inviato

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

circa un anno fa | 36 download |

4.8 / 5

Inviato

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

oltre un anno fa | 4 download |

4.0 / 5

Inviato

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

oltre un anno fa | 3 download |

5.0 / 5

Inviato

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

oltre un anno fa | 4 download |

5.0 / 5

Inviato

Moon Phases
Determination of lunar phases and checking for eclipses

oltre un anno fa | 2 download |

0.0 / 5

Inviato

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

oltre un anno fa | 1 download |

4.8 / 5

Inviato

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

oltre un anno fa | 1 download |

5.0 / 5

Inviato

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

oltre un anno fa | 4 download |

5.0 / 5

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

oltre un anno fa | 5 download |

5.0 / 5

Inviato

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

oltre un anno fa | 13 download |

5.0 / 5

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).

oltre un anno fa | 10 download |

4.9 / 5