Three-Axis Attitude Control of a Satellite in Zero Momentum Mode Using a Tilted Wheel Methodology

L.O. Inumoh, Nadjim Horri, A. Pechev, Jason Forshaw

Research output: Chapter in Book/Report/Conference proceedingConference proceeding

4 Citations (Scopus)
Original languageEnglish
Title of host publicationAIAA Guidance, Navigation and Control Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
DOIs
Publication statusPublished - Sep 2012
EventAIAA Guidance, Navigation and Control Conference - Minneapoli, United States
Duration: 13 Aug 201216 Aug 2012
https://arc.aiaa.org/doi/book/10.2514/MGNC12

Conference

ConferenceAIAA Guidance, Navigation and Control Conference
CountryUnited States
CityMinneapoli
Period13/08/1216/08/12
Internet address

Cite this

Inumoh, L. O., Horri, N., Pechev, A., & Forshaw, J. (2012). Three-Axis Attitude Control of a Satellite in Zero Momentum Mode Using a Tilted Wheel Methodology. In AIAA Guidance, Navigation and Control Conference American Institute of Aeronautics and Astronautics Inc, AIAA. https://doi.org/10.2514/6.2012-4751