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Meysam Mahooti


自 2016 起处于活动状态

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

5 hours 前 | 1997 次下载 |

5.0 / 5
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Real-Time Orbit Determination
Real-Time Orbit Determination based on GPS Navigation Data

8 days 前 | 1090 次下载 |

4.7 / 5
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已提交


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

8 days 前 | 8265 次下载 |

4.8 / 5
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Satellite Orbit Modeling
Precise modeling of a satellite's perturbed motion (special perturbations approach)

8 days 前 | 4909 次下载 |

4.1 / 5
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Relay Satellite Orbit Determination
Orbit Determination from Tracking and Data Relay Satellite Measurements

8 days 前 | 1448 次下载 |

5.0 / 5
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Reduced-Dynamic Orbit Determination
Reduced-Dynamic Orbit Determination for LEO satellites that carry a dual-frequency GPS receiver

19 days 前 | 25 次下载 |

0.0 / 5

已提交


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

1 month 前 | 18 次下载 |

0.0 / 5

已提交


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

1 month 前 | 16 次下载 |

0.0 / 5

已提交


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

1 month 前 | 27 次下载 |

0.0 / 5

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Runge-Kutta-Nystrom
Runge-Kutta-Nystrom Integration

2 months 前 | 431 次下载 |

5.0 / 5

已提交


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

3 months 前 | 151 次下载 |

0.0 / 5

已提交


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

3 months 前 | 1315 次下载 |

4.6 / 5

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

3 months 前 | 1052 次下载 |

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

3 months 前 | 2168 次下载 |

5.0 / 5
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SGP4/SDP4
SGP4 and SDP4 orbit propagators

3 months 前 | 536 次下载 |

0.0 / 5
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JPL Development Ephemerides
Computation of the position and velocity of the major planets, the Moon, and the Sun

6 months 前 | 94 次下载 |

0.0 / 5
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Satellite Orbits: Models, Methods and Applications
Satellite Orbits: Models, Methods and Applications

1 year 前 | 7019 次下载 |

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

1 year 前 | 1154 次下载 |

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

1 year 前 | 1933 次下载 |

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

1 year 前 | 1749 次下载 |

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

1 year 前 | 165 次下载 |

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

1 year 前 | 355 次下载 |

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

1 year 前 | 868 次下载 |

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

1 year 前 | 451 次下载 |

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

2 years 前 | 1703 次下载 |

5.0 / 5
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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 years 前 | 1335 次下载 |

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.

2 years 前 | 3380 次下载 |

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

2 years 前 | 603 次下载 |

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

2 years 前 | 278 次下载 |

5.0 / 5

已提交


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

2 years 前 | 1399 次下载 |

4.9 / 5
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