An academic tool intended to assist in developing an intuitive understanding of aircraft design.

Access PX4 autopilot peripherals with UAV Toolbox and automatically build and deploy flight control algorithms with Embedded Coder

Send and receive CAN messages with PEAK-System CAN devices.

Precise modeling of satellite's perturbed motion (special perturbations approach)

Spatial math primitives for MATLAB

The SGP4 model to calculate orbital state vectors of near-Earth satellites

Satellite Orbits: Models, Methods and Applications

Toolbox for angle, coordinate and date conversions and transformations. Version 2.99.

Ephemeris Data for Aerospace Toolbox

Send and receive CAN messages with Vector CAN devices.

Send and receive CAN messages with Kvaser CAN devices.

2-D nozzle using the method of characteristics and CFD on nozzle on curvilinear mesh.

This support package allows you to customize scenes in the Unreal^® Editor and use them in Simulink^®.

drawDATCOMaircraft generates an aircraft's thre view drawings from given DATCOM input files.

Standard atmosphere gas properties. Support for n-dim inputs, non-standard atmospheres, units, etc.

Solves weighted absolute orientation problem using Horn's quaternion-based method.

Opens LiDAR point data from LAS files. Supports versions up to 1.4.

Determines visibility times from observer location for specified period. LLA and KML output.

Modified SGP4 code for GPS interface

Computation of neutral temperature and densities in Earth's atmosphere from ground to thermospheric heights.

Vortex Lattice Mehod for steady aerodynamics

Modeling of satellite's perturbed motion (special perturbations approach)

Computes characteristics for coplanar and non-coplanar Hohmann transfers.

This GUI lets you plot orbits around Earth interactively.

Geoid Data for Aerospace Toolbox

Main Program to view keplerian orbit (3D) and the ground-track

Read satellite ephemeris data from a NORAD two-line element (TLE) file.

Wing Designer computes aircraft performance measures from wing and engine parameters.

A small but handy tool to quickly explore, analyse and compare airfoil geometry

This code solves the oblique shock wave relations for mach, wedge angle, or shock angle.

Transformation from celestial to terrestrial reference system and vice versa

This function plot in the same figure the center trajectory and attitude of an aircraft.

6-DOF Nonlinear Simulation of Aircraft Flight

Xfoil rewritten as MATLAB script

Case Study for DO-178 using MathWorks tools

Forward Dynamics of Planar 2-DOF Robot Manipulator for continuous time function input tau's and discrete time function input tau's

Implementations of several state-of-the-art visual saliency detection algorithms.

Convert orbital elements to a state vector, or a state vector back to orbital elements.

A GUI software I made to calculate the carrier-to-noise-density ratio of a earth-satellite link.

Draw a very simple 3D airplane and animate it too

Matlab based application to predict the orbit and track the geostationary satellites in real time.

DE405 covers 1599-12-09 to 2201-02-20. Referred to the International Celestial Reference Frame.

Calculates local Moran's I index of spatial correlation for raster.

Computes the exact solution to Sod Shock Tube problem

Function to convert rotation data between 4 types: DCM, Euler Angles, Quaternions, and Euler Param.

Example how to open and read two line element file and output six orbital elements

Simulink blockset for use with the ArduPilot Mega 2.0 hardware. Includes blocks to read external rad

Given a deflection angle, mach number, and ratio of specific heats, this function returns Beta.

Multiplying matrices, vectors, or scalars contained in two N-D arrays, with array expansion enabled.

The Albedo Toolbox provides functions for calculating the Earth albedo illuminating a spacecraft.

A MATLAB Script for Creating Pork Chop Plots of Ballistic Earth-to-Mars Trajectories

The Aircraft Library

Propagation of perturbed and unperturbed orbital trajectories from initial states

quaternion class, vectorized, converts among rotation representations, numerical Euler propagation

variation on the SPHERE command to facilitate plotting of orbital trajectories

A set of routines to make carpet plotting easier.

Full system design for narrowband smart antenna systems used in mobile communications.

Aircraft Power Network in Simscape Electrical with AC and DC networks

Compute and plot characteristics of the circular-restricted three-body problem.

Determines optimal, two-dimensional low-thrust Earth-to-Mars interplanetary trajectories.