Attitude guidance, navigation and control of land-survey mini-satellites

Ye Somov, S. Butyrin, S. Somov, C. Hajiyev

Research output: Contribution to journalConference articlepeer-review

4 Citations (Scopus)

Abstract

Contemporary land-survey mini-satellites have general mass up to 500 kg and are placed onto the orbit altitudes up to 800 km. For such spacecraft some principle problems on optimal attitude guidance, navigation and robust control are considered and elaborated methods are presented for their solving.

Original languageEnglish
Pages (from-to)222-227
Number of pages6
JournalIFAC-PapersOnLine
Volume28
Issue number9
DOIs
Publication statusPublished - 1 Jul 2015
Event1st IFAC Workshop on Advanced Control and Navigation for Autonomous Aerospace Vehicles, ACNAAV 2015 - Seville, Spain
Duration: 10 Jun 201512 Jun 2015

Bibliographical note

Publisher Copyright:
© 2015, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.

Keywords

  • Attitude control
  • Guidance
  • Mini-satellite
  • Navigation

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