Mathematical review of the attitude control mechanism for a spacecraft

Mathematical review of the attitude control mechanism for a spacecraft

The issue of inertial pointing for a spacecraft with magnetic actuators is considered and a practical global response to this problem is obtained by static attitude and speed feedback methods. A local solution dependent on dynamic attitude feedback is additionally introduced. The simulation results...

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Bibliographic Details
Main Authors: Sudhir Kumar CHATURVEDI, Saikat BANERJEE, Sourav BASU, Monika YADAV, Subhrangshu ADHIKARY
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2020-09-01
Series:INCAS Bulletin
Subjects:
euler angle
quaternion
kalman filtering (ekf
ukf)
Online Access:https://bulletin.incas.ro/files/chaturvedi_banerjee_basu_yadav---vol_12_iss_3.pdf

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