Path: OpticalNavigation/Core
% Lunar Landing NRN Sim It first creates an optimal 2D trajectory which is transformed into 3D for a north pole landing. It replicates the trajectory in a simulation. There are 3 sections: 1. Compute optimal trajectory 2. Run a simulation with the computed acceleration 3. Test optical navigation You can run each independently once all three sections have run. The simulation results are used in the Kalman Filter for testing. % -------------------------------------------------------------------------- Copyright (c) 2021 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------- Since version 2021.1 --------------------------------------------------------------------------
Missions: LunarLanding/LunarTrajectoryControl OpticalNavigation: Core/OpticalNavigation OpticalNavigation: Dynamics/RHSPlanet3DONS OpticalNavigation: Utilities/LFToECI Orbit: Visualization/PlotPlanetaryOrbit SC: BasicOrbit/Period Common: Database/Constant Common: GUIs/Figui Common: Graphics/Plot2D Common: Graphics/Plot3D Common: Graphics/TimeLabl Math: Integration/RK4 Math: Linear/Mag
Back to the OpticalNavigation Module page