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AE48726 ECTSQ2, Q3EngelsMaster

Satellite Orbit Determination

FaculteitLuchtvaart en Ruimtevaarttechniek
NiveauMaster
Studiejaar2025-2026

Beschrijving

Course contents

1 Dynamics

  • Introduction to dynamics

  • Planetary Gravity field

  • Tides and the three-body problem

  • Hill radius and Roche limit

  • Relation to planetary sciences and astrodynamics

  • Solving Equations of motion

  • Reformulate orbit problem as a system of ordinary differential equations

  • Efficiency and accuracy of numerical integration methods

  • Implementation of numerical integration methods

2 Observations techniques and reference systems

  • Observation techniques

  • Laser, Doppler, optical and VLBI observations

  • Refraction, Electromagnetism, radio- and optical technology

  • Tropospheric and ionospheric refraction

  • Relativity and the definition of time,

  • Classification of time systems (UTC, TAI, etc)

  • Light-time effect

  • Quality of clocks (Allan Variance behavior of clocks)

  • Coordinate reference systems

  • Local and global coordinate systems

  • Definition of geoid and reference ellipsoid, height systems

  • Precession and nutation, polar motion, polar wander.

  • Newton or Einstein, consequences for reference systems

3 Statistics

  • Random variables, probability density functions, moments, hypothesis testing

  • Least squares minimization

  • Unconstrained linear parameter estimation,

  • Data weighting

  • Nonlinear parameter estimation.

  • Rank deficient equation systems

  • Singular value decomposition and Empirical Orthogonal functions

  • Penrose Moore inverse

  • Compatibility conditions

  • General and homogeneous solutions

  • Constrained linear parameter estimation

  • Mechanization of parameter estimation algorithms

  • Choice of algorithms

4 Orbit determination

  • Perturbation analysis and variational problems

  • State transition matrix for initial state vector problems

  • Partial derivatives for dynamical parameters

  • Parameter estimation

  • Identification of parameters

  • Batch least squares

  • Sequential least squares: The Kalman filter, theory and implementation

5 Applications

  • Global Navigation Satellite Systems:

  • Technology and terminology,

  • Various data processing strategies and available software

  • Modeling deformation of the solid Earth,

  • The Earth's gravity field and thermospheric density

  • Satellite laser ranging and Doppler tracking via DORIS

  • Technology and terminology, results and applications

  • Observing changes in the cryosphere with satellites

  • Hydrology and Oceanography observed with satellites

6 Individual assignments in quarter 2

  • The assignments will be announced during the quarter and typically take the following form

  • One test-your-knowledge exercise related to dynamics, observation systems or reference systems

  • A graded assignment related to GNSS applied to orbit determination

  • A graded assignment related to batch or sequential least squares methods

7 Numerical Practical in quarter 3

  • Exercises with the Ghost software, typical examples are to solve:

  • Initial value problems (state vector estimation)

  • Problems with parameters in a dynamic model (drag parameter estimation)

  • Problems with time bias parameters

Toetsing

The final grade will come together from:

  1. Written examination resulting in a grade

  2. Nominally two individual assignments resulting in a weighted average grade

  3. Numerical practical resulting in "pass" or "fail".

The grading rules are as follows:

  1. The numerical practical result should be: "pass"

  2. The written examination result should be at least a 5,0

  3. In order to participate in the numerical practical you must have passed the individual assignments with at least a weighted average of 5,0

  4. No claims can be made with regard to individual assignment results or numerical practical results obtained before the previous academic year. For ae4-872 in 2025-2026 it means that results from 2024-2025 are still accepted, however, we do not accept results from 2023-2024 or earlier academic years. (Academic years run from September to August)

Due to the master curriculum refresh it is expected that ae4-872 orbit determination will run for the last time in academic year 2025-2026. This means that all course elements (exams, assignments and numerical practical) should be completed by the students in academic year 2025-2026.

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