Meysam Mahooti

自 2016 起处于活动状态

Followers: 37 Following: 0

消息

Available for projects in satellite orbit determination, astrodynamics, and astronomy. If you need my paid source code (https://www.researchgate.net/profile/Meysam-Mahooti/research), please donate in euros using the link below, then email mahooti007@gmail.com with your request. https://pay.ypaylink.com/personal-link/1322/5b99ef3b116d9f19b2442372c97af2bc059f9ed2

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

统计学

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

23 days 前 | 2008 次下载 |

5.0 / 5

已提交

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

1 month 前 | 1104 次下载 |

4.7 / 5

已提交

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

1 month 前 | 8299 次下载 |

4.8 / 5

已提交

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

1 month 前 | 4920 次下载 |

4.1 / 5

已提交

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

1 month 前 | 1456 次下载 |

5.0 / 5

已提交

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

1 month 前 | 32 次下载 |

0.0 / 5

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

2 months 前 | 21 次下载 |

0.0 / 5

已提交

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

2 months 前 | 20 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

2 months 前 | 33 次下载 |

0.0 / 5

已提交

Runge-Kutta-Nystrom
Runge-Kutta-Nystrom Integration

3 months 前 | 436 次下载 |

5.0 / 5

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

4 months 前 | 152 次下载 |

0.0 / 5

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

4 months 前 | 1316 次下载 |

4.6 / 5

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

4 months 前 | 1059 次下载 |

4.5 / 5

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

4 months 前 | 2172 次下载 |

5.0 / 5

已提交

SGP4/SDP4
SGP4 and SDP4 orbit propagators

4 months 前 | 544 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

7 months 前 | 96 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 | 7031 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 | 1162 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 | 1945 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 | 1758 次下载 |

5.0 / 5

已提交

Moon Phases
Determination of lunar phases and checking for eclipses

1 year 前 | 168 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 | 364 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 | 880 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

2 years 前 | 455 次下载 |

5.0 / 5

已提交

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

2 years 前 | 1712 次下载 |

5.0 / 5

已提交

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 | 1340 次下载 |

4.9 / 5