Satellite Orbits: Models, Methods and Applications

Versione 3.2.2 (97,8 MB) da Meysam Mahooti
Satellite Orbits: Models, Methods and Applications
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Aggiornato 25 giu 2025

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Exercise 2-1: Orbit raising using Hohmann transfer
Exercise 2-2: Solution of Kepler's equation
Exercise 2-3: Osculating elements
Exercise 2-4: Topocentric satellite motion
Exercise 2-5: Sunsynchronous repeat orbits
Exercise 2-6: Initial orbit determination (two sets of range and angle measurements of a satellite)
Exercise 3-1: Gravity field
Exercise 3-2: Lunar ephemerides
Exercise 3-3: Accelerations
Exercise 3-4: Orbit Perturbations
Exercise 4-1: Runge-Kutta 4th-order Integration
Exercise 4-2: Gauss-Jackson 4th-order predictor
Exercise 4-3: Step size control of Shampine-Gordon multistep method
Exercise 4-4: Step size control of Radau IIA multistep method
Exercise 5-1: Transformation from celestial to terrestrial reference system
Exercise 5-2: Velocity in the Earth-fixed frame
Exercise 5-3: Geodetic coordinates
Exercise 6-1: Light Time Iteration
Exercise 6-2: Range Rate Modelling
Exercise 6-3: User Clock Error from GPS Pseudorange
Exercise 6-4: Tropospheric Refraction
Exercise 7-1: State transition matrix
Exercise 8-1: Least-squares fit using Givens rotations
Exercise 8-2: Least-squares orbit determination
Exercise 8-3: Orbit Determination using Extended Kalman Filter
GEODA : Geostationary satellite Orbit Determination error Analysis
RTOD : Real Time Orbit Determination based on GPS navigation data
TDRSOD : Orbit Determination from Tracking and Data Relay Satellite measurements
References:
O. Montenbruck, and E. Gill, "Satellite Orbits: Models, Methods and Applications," Springer Verlag, Heidelberg; 2005.
Vallado D. A., "Fundamentals of Astrodynamics and Applications," McGraw-Hill, New York, 4th edition, 2013.
O. Montenbruck, and T. Pfleger, "Astronomy on the Personal Computer," Springer Verlag, Heidelberg, 4th edition, 2000.
https://ssd.jpl.nasa.gov/planets/eph_export.html
http://celestrak.org/SpaceData/EOP-All.txt
http://celestrak.org/SpaceData/SW-All.txt

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Meysam Mahooti (2025). Satellite Orbits: Models, Methods and Applications (https://it.mathworks.com/matlabcentral/fileexchange/55533-satellite-orbits-models-methods-and-applications), MATLAB Central File Exchange. Recuperato .

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Satellite Orbits_Models, Methods, and Applications_3.2.2

Versione Pubblicato Note della release
3.2.2

It was revised on 2025-06-24.
3.2.1

It was revised on 2025-04-14.
3.2.0

It was revised on 2024-12-14.
3.1.2

Range_4W.m was modified.
3.1.1

It was revised on 2022-10-30.
3.1.0

It was revised on 2022-09-24.
3.0.0.0

The Accel_Grad.m is modified.
2.2.2.2

Modifications are made to SAT_Const.m, AccelHarmonic_AnelasticEarth.m, and AccelHarmonic_ElasticEarth.m.
2.2.2.1

The AccelHarmonic_AnelasticEarth.m, the AccelHarmonic_ElasticEarth.m, and the Accel.m are modified.
2.2.1.1

Mjday_TDB.m and nrlmsise00.m are modified.
2.2.1.0

The DE430 full matrix is added.
2.1.1.0

Exercise_3_2.m, Exercise_8_2.m, and Exercise_8_3.m are modified.
2.1.0.0

Revised on March 26, 2020.
2.0.0.0

Revised on 2018-01-27.
1.1.0.0

TDRSOD.m and Trj.m are changed to decrease the CPU time.
NRLMSISE00 atmospheric density model is replaced by modified Harris-Priester model.
Low precision analytical lunar ephemeris is replaced by Brown's theory (Improved Lunar Ephemeris) and JPL precise ephemeris.
The image is added.
Revised on 2016-11-17.
Computation of state transition matrix (Exercise_7_1.m) is improved to decrease CPU time.
TDRSOD.m and Trj.m are changed to decrease the CPU time.
Modified Harris-Priester model is replaced by NRLMSISE00 atmospheric density model.
Density_nrlmsise00.m is improved.
1.0.0.0