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

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

Satellite Orbits: Models, Methods and Applications

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

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

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

The Aircraft Library

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

中性温度和密度的计算n Earth's atmosphere from ground to thermospheric heights.

variation on the SPHERE command to facilitate plotting of orbital trajectories

Draw a very simple 3D airplane and animate it too

Xfoil rewritten as MATLAB script

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

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

Computes characteristics for coplanar and non-coplanar Hohmann transfers.

Modified SGP4 code for GPS interface

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

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

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

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.

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

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

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

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

This GUI lets you plot orbits around Earth interactively.

Implementation of Levy's flight

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

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

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

This library provides blocks to communicate with the flight Simulator X-Plane.

Geoid Data for Aerospace Toolbox

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

A set of routines to make carpet plotting easier.

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.

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

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

An easy-to-use tool to optimize trajectories for interplanetary missions using swingby manoevres

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

6-DOF Nonlinear Simulation of Aircraft Flight

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

Generates the NACA 5 digit airfoil coordinates

Apollo Lunar Module model

Propagation of perturbed and unperturbed orbital trajectories from initial states

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

MAS

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

Generates an airfoil shape using CST method

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

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

This program decodes the data from an IMU.

Design a two-body, low-thrust spiral trajectory with a constant periapsis radius.

Simple design for helicopter control system

从跟踪和数据重新定轨lay Satellite Measurements

Aircraft Power Network in Simscape Electrical with AC and DC networks

This software was released by Princeton Satellite Systems, Inc.

Visualization, Transformation and 0°-45°-90° Strain Gage Rosette Evaluation

A Modular Simulation Environment for the Improved Dynamic Simulation of Multirotor UAVs

Demonstrates how to model the trajectory of aerospace vehicles in the flight path coordinate system.