The reference applications are fully realized aerospace models, including hybrid and electric aircraft and CubeSats, and flight analysis.
|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|
|Start flight control analysis template|
|Calculate dutch roll mode, roll mode, and spiral mode characteristics of state-space model|
|Calculate short-period and long-period (phugoid) mode characteristics of specified state-space model|
|Linearize airframe model around operating points|
|Trim airframe around operating point specification object|
Get started with CubeSats.
Model, simulate, analyze, and visualize the motion and dynamics of CubeSats.
Analyze CubeSat mission geometries.
Analyze dynamic response and flying qualities of aerospace vehicles using flight control analysis tools.
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.