CubeSats

Model, simulate, analyze, and visualize the motion and dynamics of CubeSats; analyze CubeSat missions

Model, simulate, analyze, and visualize the motion and dynamics of CubeSats using the CubeSat Vehicle block and related functions. Analyze CubeSat missions using a live script. Install the CubeSat Simulation Library as an add-on using the Add-On Explorer in the MATLAB® desktop.

Functions

asbAddOnsStart Add-On Explorer for aerospace Add-Ons
asbCubeSatMissionAnalysisCreate and launch new instance of CubeSat Mission Analysis live script
ecef2eciPosition and velocity vectors in Earth-centered inertial mean-equator mean-equinox
eci2ecefPosition, velocity, and acceleration vectors in Earth-centered Earth-fixed (ECEF) coordinate system
generateAccessTableCalculate line-of-sight (LOS) mutual visibility between CubeSat vehicle and ground station
greenwichsrtGreenwich mean and apparent sidereal times
ijk2keplerianKeplerian orbit elements using position and velocity vectors
keplerian2ijkPosition and velocity vectors in geocentric equatorial coordinate system using Keplerian orbit elements

Blocks

CubeSat VehicleModel CubeSat vehicle

Topics

Getting Started with CubeSats

Get started with CubeSats.

Model and Simulate CubeSats

Model, simulate, analyze, and visualize the motion and dynamics of CubeSats.

Analyze CubeSat Mission Geometry

Analyze CubeSat mission geometries.