tudat.space
stable
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
Impact Manifolds of Lagrange Point Orbits in CR3BP(-Polyhedron)
Keplerian satellite orbit
Linear sensitivity analysis of perturbed orbit
Multiple Gravity Assist trajectories
Perturbed satellite orbit
Re-entry trajectory
Separation of satellites via differential drag
Solar System Propagation
Two-stage rocket ascent
Covariance analysis of estimated parameters
Cassini 1 (MGA transfer) optimization with PyGMO
Himmelblau minimization with PyGMO
Hodographic-shaping MGA transfer optimization with PyGMO
Asteroid orbit optimization with PyGMO - Custom Environment
Asteroid orbit optimization with PyGMO - Design Space Exploration
Asteroid orbit optimization with PyGMO - Optimization
Tudatpy Submodules
User guide
State Propagation
Environment Setup
Creating and modifying the bodies
Creation of celestial body settings
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
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
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
Observation models
Observation Simulation
Estimation Settings
Performing the estimation
Preliminary Mission Design
Multiple Gravity Assists Transfer
Mathematics
Interpolators
Advanced topics
Post-processing Results in Python
Optimization with PyGMO
About
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Research output
History
tudat.space
Index
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Index
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Q
Quaternions (built-in class)
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v: stable
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