Programming Languages:
MATLAB
Spoken Languages:
English
Professional Interests:
Numerical Integration and Differential Equations, Aerospace, Satellite and Orbital Mechanics
MATLAB
Spoken Languages:
English
Professional Interests:
Numerical Integration and Differential Equations, Aerospace, Satellite and Orbital Mechanics
Feeds
已提交
NASA JPL Development Ephemerides (DE405)
DE405 covers 1599-12-09 to 2201-02-20. Referred to the International Celestial Reference Frame.
6 days 前 | 27 次下载 |
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Initial orbit determination
Initial orbit determination (two sets of range and angle measurements of a satellite)
14 days 前 | 9 次下载 |
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Satellite Visibility
Propagation of the satellite's state vector using SGP4 and checking its visibility for future
15 days 前 | 15 次下载 |
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Initial Orbit Determination (Least Squares Method)
Initial orbit determination applying the Least Squares method
2 months 前 | 24 次下载 |
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Initial Orbit Determination (Angles-Only Method)
Angles-only approach applying the Least Squares method
2 months 前 | 14 次下载 |
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NASA JPL Development Ephemerides (DE440)
High precision planetary ephemerides
2 months 前 | 9 次下载 |
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NASA JPL Development Ephemerides (DE441)
High-precision computation of planetary ephemerides
4 months 前 | 16 次下载 |
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Lambert's Problem
Lambert’s problem is the orbital boundary-value problem constrained by two points and elapsed time.
4 months 前 | 19 次下载 |
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ECEF2ECI & ECI2ECEF Transformations_IAU 2006 Resolutions
Transformation from terrestrial to celestial reference system and vice versa
7 months 前 | 6 次下载 |
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ECI2ECEF & ECEF2ECI Transformations
Transformation from celestial to terrestrial reference system and vice versa
7 months 前 | 30 次下载 |
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Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times
7 months 前 | 5 次下载 |
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Sunrise Sunset
Rising and setting times of the Sun and the Moon and twilight times
7 months 前 | 7 次下载 |
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Initial Orbit Determination (Extended Kalman Filter)
Initial orbit determination applying the Extended Kalman Filter
8 months 前 | 13 次下载 |
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Double-r Initial Orbit Determination
Double-r method is utilized to determine the initial orbit.
8 months 前 | 5 次下载 |
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Gauss Initial Orbit Determination
Gauss's method is utilized to determine the initial orbit.
8 months 前 | 9 次下载 |
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SGP4
The SGP4 model to calculate orbital state vectors of near-Earth satellites
8 months 前 | 75 次下载 |
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High Precision Orbit Propagator
Precise modeling of satellite's perturbed motion (special perturbations approach)
8 months 前 | 80 次下载 |
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Satellite Orbit Modeling
Modeling of satellite's perturbed motion (special perturbations approach)
8 months 前 | 32 次下载 |
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JPL Development Ephemerides
Computation of position and velocity of major planets, the Moon, and the Sun
11 months 前 | 2 次下载 |
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Solar Eclipse
Prediction of solar eclipse and its duration using the time of new moon
11 months 前 | 20 次下载 |
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Jacchia-Bowman Atmospheric Density Model
Computation of the total mass-desnity of atmosphere using Jacchia-Bowman model
1 year 前 | 12 次下载 |
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Modified Jacchia 70
Computation of atmospheric density for drag effect modeling
1 year 前 | 5 次下载 |
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Sun/Moon Rise/Set
Rising and setting times of the Sun and the Moon and twilight times
1 year 前 | 4 次下载 |
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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 | 4 次下载 |
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Moon Position
Position of the Moon referred to the mean equator and equinox of J2000
1 year 前 | 15 次下载 |
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Sun Position (VSOP87)
VSOP87 defines the analytical solutions to the motions of the solar system planets
1 year 前 | 5 次下载 |
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Sun Position
Geocentric equatorial position of the Sun (in [m]), referred to the ICRF
1 year 前 | 16 次下载 |