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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.
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An innovation project to explore the feasibility of reconfigure the position of attitude actuators (reaction wheels) in order to control the orientation of a 3U CubeSat satellite.
RotEx is a set of python helper functions to apply 3D rotation, like Euler Angles etc, based on scipy.spatial.transform.Rotation. You can learn, understand and test Rotation quickly, and use these functions in your codes easily.
A project to find a convenient mathematical model that allows to get the optimal mechanical design of a non-COTS reaction wheel for a 3U CubeSat attitude control.
Research project where was developed a new Guidance, Navigation and Control (GNC) law for Attitude Determination and Control Systems (ADCS) of CubeSat satellites.