Developed a missile guidance and ballistic control system for autonomous mid-air and surface-to-air target chase and interception
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Updated
Dec 30, 2022 - MATLAB
Developed a missile guidance and ballistic control system for autonomous mid-air and surface-to-air target chase and interception
Demonstration of Conventional 2 Sensor Attitude Determination using VRML in Simulink
Interactive courseware that introduces foundational-level concepts as taught in introductory courses in fluid mechanics.
Algorithms regarding spacecraft attitude determination and control.
Simple J2 propagator modeled in Simulink
This repository contains the source code for a modified Beddoes-Leishman dynamic stall model
Educational Vibration programs for Octave. Intended for undergraduate and early graduate students.
PteraControls is a tool for designing control systems for flapping wing vehicles.
A program to calculate the parameters of a turbofan engine (Matlab).
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.
Computes the contours of a 2D minimum-length supersonic nozzle for non-rotating flows using the method of the characteristics.
SLOSH-ML is a Matlab graphical user interface designed to analyze rocket propellant sloshing in space launch vehicles
Numerical and Analytical Flow Solution over Joukowski Aerofoil, Using O-grid Meshing Method and PSOR solving algorithm.
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.
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