Development of SPEL - Open Star Tracker (SOST) - Software tested in our nanosatellites SUCHAI-2/3 AND PlantSAT

Implementations of the major developments in 3D-attitude determination of spacecraft including the Triad method and various solutions to the Wahba's problem.

Development of star simulator software for star sensor research.

Demonstration of Conventional 2 Sensor Attitude Determination using VRML in Simulink

Attitude Determination System for SFU Satellite Design Team

Design, Construction and Programming of a hemispherical air bearing supported satellite with attitude control using an IMU, sun tracking, telemetry/telecommand communication(SPI/UART) and docking capabilities.

Dataset as a part of DIALOG'2018 paper: "Extracting Sentiment Attitudes From Analytical Texts"

GNSS single antenna attitude determination

Developed an algorithm for Attitude Determination and control of a 1DOF 1U Cubesat.

Creating a neural-network based star pattern recognition system

This is the main repository for the codes for Spacecraft Attitude Control course Final Project - Politecnico di Milano

Cubesat ADCS code written by Zarvan Movdawalla and Team, from MPSTME Mumbai.

Assignment for Spacecraft Attitude Dynamics and Control course at Politecnico di Milano, academic year 2020-2021.

Simulation of satellite attitude dynamics, determination and control using simulink; considering sensor errors

estimator to minimize Wahba's loss function for satellite attitude

WORK IN PROGRESS - Within course SD2910 of MSc KTH, relying on book.

Main repository for the codes for the final project of the course ' Spacecraft attitude dynamics' at Politecnico di Milano

Simulator of Attitude Control System for "ITF-3"

Rede neural para determinação da atitude de satélites.