Actuator modelling for attitude control using incremental nonlinear dynamic inversion
01.01.2020
1-9 pages
International journal of micro air vehicles 12, 1-9 (2020). doi:10.1177/1756829320961925
Sonstige
Elektronische Ressource
Englisch
Robust Nonlinear Spacecraft Attitude Control using Incremental Nonlinear Dynamic Inversion
British Library Conference Proceedings | 2012
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