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 conferencePaperpeer-review

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
DOIs
Publication statusPublished - 13 Aug 2012

Bibliographical note

AIAA Guidance, Navigation, and Control Conference ; Conference date: 13-08-2012 Through 16-08-2012

Keywords

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

Cite this