Demonstration of Conventional 2 Sensor Attitude Determination using VRML in Simulink
-
Updated
Aug 26, 2017 - MATLAB
Demonstration of Conventional 2 Sensor Attitude Determination using VRML in Simulink
Assignment for Spacecraft Attitude Dynamics and Control course at Politecnico di Milano, academic year 2020-2021.
This code is a simple implementation of Incremental Nonlinear Dynamics Inversion (INDI) algorithm for quadrotor attitude control. It is inspired from the paper: Coelho, Rodrigo, Alexandra Moutinho, and José Raul Azinheira. "Quadrotor Attitude Control using Incremental Nonlinear Dynamics Inversion." ICINCO (2). 2017.
Add a description, image, and links to the attitude topic page so that developers can more easily learn about it.
To associate your repository with the attitude topic, visit your repo's landing page and select "manage topics."