Design and Implementation of Attitude Control System for Gnssas 6U Cubesat

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Citations (Scopus)

Abstract

This paper studies the attitude determination and control system (ADCS) of the GNSSaS CubeSat. It investigates the disturbance analysis, the B-dot algorithm for the detumbling mode, and the PID controller for the nadir pointing mode. The analysis identified various types of disturbances that can impact the CubeSat's attitude control system and simulated their effects. The results shows that the implementation of the B-dot algorithm demonstrated good performance in detumbling the GNSSaS. The PID controller for Nadir pointing mode achieved the mission requirement which is to have a pointing stability of less than 0.1 deg/sec. Overall, the findings of this study offer valuable insights for optimizing the attitude control system of CubeSats for different missions.

Original languageEnglish
Title of host publicationIGARSS 2023 - 2023 IEEE International Geoscience and Remote Sensing Symposium, Proceedings
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages384-387
Number of pages4
ISBN (Electronic)9798350320107
DOIs
Publication statusPublished - 2023
Event2023 IEEE International Geoscience and Remote Sensing Symposium, IGARSS 2023 - Pasadena, United States
Duration: Jul 16 2023Jul 21 2023

Publication series

NameInternational Geoscience and Remote Sensing Symposium (IGARSS)
Volume2023-July

Conference

Conference2023 IEEE International Geoscience and Remote Sensing Symposium, IGARSS 2023
Country/TerritoryUnited States
CityPasadena
Period7/16/237/21/23

Keywords

  • ADCS
  • B-dot
  • Control
  • CubeSat
  • PID

ASJC Scopus subject areas

  • Computer Science Applications
  • General Earth and Planetary Sciences

Fingerprint

Dive into the research topics of 'Design and Implementation of Attitude Control System for Gnssas 6U Cubesat'. Together they form a unique fingerprint.

Cite this