Attitude estimation of a small spinning satellite using Kalman filter approaches

Osama Khurshid

Research output: ThesisDoctoral ThesisMonograph

Original languageEnglish
QualificationDoctor's degree
Awarding Institution
  • Aalto University
Supervisors/Advisors
  • Kallio, Esa, Supervising Professor
  • Selkäinaho, Jorma, Thesis Advisor
Publisher
Print ISBNs978-952-60-7503-7
Electronic ISBNs978-952-60-7504-4
Publication statusPublished - 2017
MoE publication typeG4 Doctoral dissertation (monograph)

Keywords

  • satellite
  • spacecraft
  • attitude dynamics
  • system design
  • Kalman filter
  • UKF
  • PSLKF

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