TU Delft Astrodynamic Toolbox

Contents

  • Start Page
  • Getting Started
  • Installation Guide
  • Tutorials and Documentation
    • Application Tutorials
    • Tudat Libraries
      • 1. Environment Set-up
      • 2. Setting up State Derivative Models
      • 3. Simulator Set-Up
      • 4. Estimation Set-Up
      • 5. Basic Astrodynamics Tools
        • 5.1. Frame/State Transformations
        • 5.2. Mission Segments
        • 5.3. Trajectory Design
      • Low-Thrust Trajectory Design Module
      • 6. Basic Mathematics Tools
      • 7. Other Libraries
    • Tudat Basics
    • JSON Interface
    • MATLAB Interface
    • Doxygen
    • Troubleshooting
  • FAQ
  • Developer Guide
TU Delft Astrodynamic Toolbox
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  • 5. Basic Astrodynamics Tools
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5. Basic Astrodynamics Tools¶

These pages of the wiki will help you build a strong knowledge basis to get started with Tudat. These pages will give you and introduction into the astrodynamical tools that are available in Tudat.

  • 5.1. Frame/State Transformations
    • 5.1.1. State Type Conversions
      • 5.1.1.1. Kepler Elements
      • 5.1.1.2. Spherical-orbital Elements
      • 5.1.1.3. Modified Equinoctial Elements
      • 5.1.1.4. Unified State Model Elements
      • 5.1.1.5. Quaternions
      • 5.1.1.6. Modified Rodrigues Parameters
      • 5.1.1.7. Exponential Map
    • 5.1.2. Frame Transformations
      • 5.1.2.1. Frame Translations
      • 5.1.2.2. Frame Rotations
  • 5.2. Mission Segments
    • 5.2.1. Lambert Targeter
  • 5.3. Trajectory Design
    • 5.3.1. Trajectory Models
    • 5.3.2. Trajectory Calculation
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