The reference applications are fully realized aerospace models, including hybrid and electric aircraft and CubeSats.
|Start Add-On Explorer for aerospace Add-Ons|
|Create and launch new instance of CubeSat Mission Analysis live script|
|Position and velocity vectors in Earth-centered inertial mean-equator mean-equinox|
|Position, velocity, and acceleration vectors in Earth-centered Earth-fixed (ECEF) coordinate system|
|Calculate line-of-sight (LOS) mutual visibility between CubeSat vehicle and ground station|
|Greenwich mean and apparent sidereal times|
|Keplerian orbit elements using position and velocity vectors|
|Position and velocity vectors in geocentric equatorial coordinate system using Keplerian orbit elements|
Get started with CubeSats.
Model, simulate, analyze, and visualize the motion and dynamics of CubeSats.
Analyze CubeSat mission geometries.
This example illustrates how to use modeling for rapid exploration of design space in the hybrid and electric aircraft area and compare the results to design criteria.