Nanosatellite air bearing tests of fault-tolerant sliding-mode attitude control with unscented kalman filter

Mark Post, Junquan Li, Regina Lee

Research output: Contribution to conferencePaper

6 Citations (Scopus)
230 Downloads (Pure)

Abstract

This paper documents the development and testing of a fault tolerant sliding mode attitude control algorithm for a nanosatellite with reaction wheel control actuation.
Original languageEnglish
Number of pages12
DOIs
Publication statusPublished - 13 Aug 2012
EventAIAA Guidance, Navigation, and Control Conference - Hyatt Regency, Minneapolis, United States
Duration: 13 Aug 201216 Aug 2012

Conference

ConferenceAIAA Guidance, Navigation, and Control Conference
CountryUnited States
CityMinneapolis
Period13/08/1216/08/12

Keywords

  • nanosatellite
  • air bearing tests
  • fault-tolerant
  • sliding mode attitude control
  • unscented Kalman filter

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  • Cite this

    Post, M., Li, J., & Lee, R. (2012). Nanosatellite air bearing tests of fault-tolerant sliding-mode attitude control with unscented kalman filter. Paper presented at AIAA Guidance, Navigation, and Control Conference, Minneapolis, United States. https://doi.org/10.2514/6.2012-5040