Demonstration of Conventional 2 Sensor Attitude Determination using VRML in Simulink
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Updated
Aug 26, 2017 - MATLAB
Demonstration of Conventional 2 Sensor Attitude Determination using VRML in Simulink
Computes the contours of a 2D minimum-length supersonic nozzle for non-rotating flows using the method of the characteristics.
A program to calculate the parameters of a turbofan engine (Matlab).
Simple J2 propagator modeled in Simulink
Algorithms regarding spacecraft attitude determination and control.
The study aims to develop a preliminary design of a fixed-wing aerodyne (Business Jet) able to carry a reduced number of people in intercontinental flights at the maximum possible Mach number.
Educational Vibration programs for Octave. Intended for undergraduate and early graduate students.
Interactive courseware that introduces foundational-level concepts as taught in introductory courses in fluid mechanics.
Developed a missile guidance and ballistic control system for autonomous mid-air and surface-to-air target chase and interception
Numerical and Analytical Flow Solution over Joukowski Aerofoil, Using O-grid Meshing Method and PSOR solving algorithm.
PteraControls is a tool for designing control systems for flapping wing vehicles.
Programi iz knjige Stajni trap letelica.
My matlab code (Numerical Analysis, Simulation)
Simple software created to quickly output aircraft landing gear design geometry during a year long iterative design process. This allowed for complex trade off analysis with other design team members.
SLOSH-ML is a Matlab graphical user interface designed to analyze rocket propellant sloshing in space launch vehicles
This repository contains the source code for a modified Beddoes-Leishman dynamic stall model
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