Skip to main content
Ctrl+K
Have questions or feedback? Let us know in our Github Discussion forum!
tudat.space 0.9.0 documentation - Home tudat.space 0.9.0 documentation - Home
  • Getting Started
  • Examples
  • User Guide
  • API Reference
  • About
  • Getting Started
  • Examples
  • User Guide
  • API Reference
  • About

Section Navigation

Tudat(Py) 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
    • 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
      • Available Observation Models
    • Observation Creation
      • Loading Real Tracking Data
    • Estimation Settings
    • Performing the estimation
  • Preliminary Mission Design
    • Multiple Gravity Assists Transfer
  • Mathematics
    • Interpolators
  • Mathematical model definition
  • TudatPy Submodules

Interface with other libraries

  • Optimization with PyGMO
  • Parallelization with Python
  • Post-processing Results in Python
  • User Guide
  • Mathematics

Mathematics#

Tudat contains various pieces of functionality of a purely mathematical nature, which are used to support the astrodynamics calculations. The setup of numerical integrators is discussed in the context of numerical state propagation. Below, additional mathematical functionality is documented.

  • Interpolators
    • General procedure
    • Available types of interpolators
    • Additional settings

previous

Multiple Gravity Assists Transfer

next

Interpolators
Edit on GitHub

This Page

  • Show Source

© Copyright 2025, Tudat Team.

Created using Sphinx 7.4.7.

Built with the PyData Sphinx Theme 0.16.1.