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

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

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

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

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

Satellite Orbits: Models, Methods and Applications

Vortex Lattice Mehod for steady aerodynamics

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

Send and receive CAN messages with Vector CAN devices.

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.

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

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

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

Ephemeris Data for Aerospace Toolbox

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

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

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

variation on the SPHERE command to facilitate plotting of orbital trajectories

Draw a very simple 3D airplane and animate it too

Modified SGP4 code for GPS interface

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

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

Xfoil rewritten as MATLAB script

Transformation from celestial to terrestrial reference system and vice versa

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

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

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

Computes characteristics for coplanar and non-coplanar Hohmann transfers.

Send and receive CAN messages with Kvaser CAN devices.

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

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

compute gas turbine engine performance under varying operating condition.

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

Case Study for DO-178 using bat365 tools

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

Example that shows how you can visualize airline routes on the globe.

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

This GUI lets you plot orbits around Earth interactively.

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

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

Computes the exact solution to Sod Shock Tube problem

Convert latitude, longitude,altitude to earth-centered, earth-fixed (ECEF) cartesian coordinate.

Geoid Data for Aerospace Toolbox

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

A MATLAB Script for Interplanetary Gravity-Assist Trajectory Design and Optimization

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

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

Vectorized quaternion functions

Educating tool for understanding the complicated Helicopter blade motions & various reference planes

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

Source Panel Method applied to Flow around Cylinder. Example 3.19 from Anderson's book

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

A GUI application which conducts cycle analysis on a turbojet engine.

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

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

6-DOF Nonlinear Simulation of Aircraft Flight