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

Spatial math primitives for MATLAB

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

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

Computes characteristics for coplanar and non-coplanar Hohmann transfers.

Satellite Orbits: Models, Methods and Applications

Xfoil rewritten as MATLAB script

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

Vortex Lattice Mehod for steady aerodynamics

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

A set of routines to make carpet plotting easier.

Ephemeris Data for Aerospace Toolbox

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

This potential flow simulator simulates the flow past bodies of arbitrary shape including airfoils.

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

variation on the SPHERE command to facilitate plotting of orbital trajectories

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

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

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

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

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

This GUI lets you plot orbits around Earth interactively.

Simulink library of aircraft models

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

Beta(s) are plotted for range of theta(s) varying with specific upstream supersonic Mach number(s) highlighting the values of max. theta(s).

Computes the exact solution to Sod Shock Tube problem

Transformation from celestial to terrestrial reference system and vice versa

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

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

With an input section, giving as output a number of variables useful for a pre-design of a wing.

Geoid Data for Aerospace Toolbox

Case Study for DO-178 using MathWorks tools

A set of functions for processing Mark Drela's AVL and XFoil data

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

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

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

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

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

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

6-DOF Nonlinear Simulation of Aircraft Flight

Calculates Temperature, Pressure, Density, Speed of Sound, Gravity, Dynamic/Kinematic Viscosity, k,

Mohr's circle for a general three-dimensional state of stresses

Modified SGP4 code for GPS interface

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

Satellite Propagation with Runge-Kutta 4th Order Numerical Integration Method

Draw a very simple 3D airplane and animate it too

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

Calculates the maximum pressure the composite can withstand and other properties.

Satellite Orbit Transfer Simulation

compute gas turbine engine performance under varying operating condition.

Aircraft Power Network in Simscape Electrical with AC and DC networks

Visualize orbit trajectory around earth

Generates an airfoil shape using CST method

Generates the NACA 5 digit airfoil coordinates

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

A compilation of all of the functions I wrote for my orbital mechanics class

Calculates various flow relations for compressible fluid flow

Analyses all combination of plies within a specified interval and a given increment to find the most strongest laminate.

Example how to simulate an unmanned glider and extract flight dynamics for trimmed gliding.