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Tudatpy example categories

  • Propagation
    • Keplerian satellite orbit
    • Perturbed satellite orbit
    • Linear sensitivity analysis using variational equations
    • Solar System Propagation using Multi-Body Dynamics
    • Thrust between the Earth and the Moon
    • JUICE Flybys of Jovian Moons
    • Setup a Panelled Radiation Pressure Model
    • Re-entry trajectory using custom aerodynamic guidance
    • Two-stage rocket ascent
    • Separation of satellites via differential drag
    • Basic thrust model for satellite engines
    • Propagation of coupled translational-rotational dynamics
    • Impact Manifolds of Lagrange Point Orbits in CR3BP(-Polyhedron)
  • Estimation
    • Covariance Analysis with DELFI-C3
    • Covariance Propagation Using Starlink-32101
    • Parameter Estimation with DELFI-C3
    • Simulation and Estimation Using Different Dynamical Models
    • Generating Visibility Plots with Tudat
    • Objectives
    • Initial State Estimation Using NOE-5 Ephemeris
    • Retrieving Observations From the Minor Planet Centre
    • Initial state estimation From Real MPC Observations
    • Improved state estimation with MPC
    • Loading and Using Tracking Observations
    • Objectives
    • MRO - Comparing Doppler and range measurements from ODF files to simulated observables
    • GRAIL - Estimating the spacecraft trajectory from ODF Doppler measurements
    • GRAIL - Comparing Doppler measurements from ODF files to simulated observables
    • GRAIL - Fitting various models of the GRAIL spacecraft’s dynamics to the reference spice trajectory
  • Mission Design
    • Multiple Gravity Assist trajectories
    • Earth-Mars transfer window design using Porkchop Plots
    • Earth-Mars transfer window design using Porkchop Plots
    • Hodographic-shaping MGA transfer optimization with PyGMO
    • Cassini 1 (MGA transfer) optimization with PyGMO
  • Optimization using PyGMO
    • 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
  • Examples
  • Optimization using PyGMO

Optimization using PyGMO#

Note

If you have never used PyGMO before, please consider reading our introductory guide: Optimization with PyGMO.

Optimization with PyGMO#

Below, a number of examples of Tudat applications used the Pygmo optimization toolbox are shown. Note that a number of additional related examples are given on the page for Trajectory optimization.

Himmelblau minimization with PyGMO
Asteroid Orbit Optimization

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Cassini 1 (MGA transfer) optimization with PyGMO

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Himmelblau minimization with PyGMO
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