This document describes the implementation of a state estimator, and an attitude controller for Advitiy, IIT Bombay’s 2nd Student Satellite. The algorithms used by the estimator and the controller are described. A closed-loop simulation (CLS) framework for the testing of these algorithms is explained. A detailed description of each of the blocks in CLS framework has been provided. The problems faced due to actuation with magnetorquer are described. It also contains the description of practices followed to ensure the quality (correctness of results obtained and repeatability of the process).


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Closed-Loop Simulation for Attitude Control of Nano-satellite


    Additional title:

    Lect.Notes Mechanical Engineering


    Contributors:


    Publication date :

    2020-05-05


    Size :

    11 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




    Closed-Loop Simulation for Attitude Control of Nano-satellite

    Riya / Chirame, Sanket / Joshi, Anant A. et al. | TIBKAT | 2020


    Flight Demonstration of Stealthy Closed-Loop Attitude Control

    A. B. Cain / T. T. Ng / E. J. Kerschen et al. | NTIS | 2002


    Minimal Configuration Attitude Control for Nano Satellite

    Mualem, S. / Verbin, D. / Tekhniyon, Makhon tekhnologi le-Yisra'el | British Library Conference Proceedings | 2011


    A Closed-Loop Hardware Simulation of Decentralized Satellite Formation Control

    Ebimuma, Takuji / Lightsey, E. Glenn / Baur, Frank | NTRS | 2002