Power Analysis of Optimal Earth Observation Micro-Satellite Design under Different Control Parameter

Muhammad Sulaiman Nur Ubay, Abdul Halim

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The main task of an earth observation satellite is to deliver accurate and valid earth surface information to the ground station. In order to perform this task, the satellite is equipped with an attitude control system. The control system establishes closed-loop with attitude sensors, especially in the imaging operation. However, the limitation of satellite power supply capacity causes the restriction of attitude control operation, which in turn, limits the satellite imaging capacity. The aim of this paper is to analyze the power performance of optimal satellite design by observing the effects of a Proportional Integral Differential (PID) parameter changes to satellite power consumption. In this paper, firstly optimal satellite parameters are chosen. The parameter choice is based on a quadratic objective function that representing power consumption. In the sequence, the PID attitude control system is designed for the satellite. Through simulation, the effects of various PID parameters have been studied.

Original languageEnglish
Title of host publicationICARES 2018 - Proceedings of the 2018 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages134-139
Number of pages6
ISBN (Electronic)9781538660324
DOIs
Publication statusPublished - 26 Nov 2018
Event2018 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology, ICARES 2018 - , Indonesia
Duration: 20 Sep 201821 Sep 2018

Publication series

NameICARES 2018 - Proceedings of the 2018 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology

Conference

Conference2018 IEEE International Conference on Aerospace Electronics and Remote Sensing Technology, ICARES 2018
Country/TerritoryIndonesia
Period20/09/1821/09/18

Keywords

  • attitude control system
  • imaging operation
  • PID
  • power supply capacity
  • satellite

Fingerprint

Dive into the research topics of 'Power Analysis of Optimal Earth Observation Micro-Satellite Design under Different Control Parameter'. Together they form a unique fingerprint.

Cite this