tudat.space
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Getting started
Installation
Setting Up a Development Environment
Primers for coding tools
Getting Started with Conda
Getting Started with Python
Getting started with Git
Examples
Propagation Examples
Keplerian satellite orbit
Linear sensitivity analysis of perturbed orbit
Perturbed satellite orbit
Solar System Propagation
Thrust between the Earth and the Moon
Re-entry trajectory
Separation of satellites via differential drag
Propagation of coupled translational-rotational dynamics
Impact Manifolds of Lagrange Point Orbits in CR3BP(-Polyhedron)
Estimation Examples
DELFI-C3 - Covariance Analysis
DELFI-C3 - Parameter Estimation
MARS EXPRESS - Dynamical Model Error
Galilean Satellites - Initial State Estimation
Retrieving observation data from the Minor Planet Centre
Initial state estimation with Minor Planet Center Observations
Mission Design Examples
Multiple Gravity Assist trajectories
Earth-Mars transfer window design using Porkchop Plots
Hodographic-shaping MGA transfer optimization with PyGMO
Cassini 1 (MGA transfer) optimization with PyGMO
PyGMO Examples
Himmelblau minimization with PyGMO
Asteroid Orbit Optimization
Asteroid orbit optimization with PyGMO - Custom Environment
Asteroid orbit optimization with PyGMO - Design Space Exploration
Asteroid orbit optimization with PyGMO - Optimization
Tudatpy Submodules
Frequently Asked Questions
Using the Tudat source code
User guide
State Propagation
Environment Setup
Creating the bodies
Modifying the bodies
Environment Models
Default environment models
Default bodies with a limited valid time range
Custom models
Interacting with the environment during propagation
Frames in the Environment
Times and dates
Available State Definitions and Conversions
Environment - Overall Architecture
Thrust and Aerodynamic Orientation - Code Refactor
Use of thrust models - Legacy
Propagation Setup
Translational Dynamics
Acceleration Model Setup
Available Acceleration Models
Third-body accelerations
Radiation pressure acceleration
Use of thrust models
Use of aerodynamics
Rotational Dynamics
Torque Model Setup
Available Torque Models
Mass Dynamics
Multi-type dynamics
Multi-body dynamics
Multi- and hybrid-arc dynamics
Processed vs. Propagated State Elements
Integration Setup
Termination Settings
Dependent Variables
Printing and processing the results
Propagating Dynamics
Propagation results
Propagation architecture
Propagating Variational Equations
Parameter Settings
Available Parameters
Single-arc Variational Equations Propagation
State Estimation
Link Ends Setup
Observation Model Setup
Avalailable Observation Models
Observation Creation
Loading Real Tracking Data
Estimation Settings
Performing the estimation
Preliminary Mission Design
Multiple Gravity Assists Transfer
Mathematics
Interpolators
Advanced topics
Post-processing Results in Python
Parallelization with Python
Optimization with PyGMO
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Quaternions (built-in class)
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