Model Predictive Control of a Tandem-Rotor Helicopter With a Nonuniformly Spaced Prediction Horizon
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DOI: 10.1109/lcsys.2022.3178785
Abstract: This letter considers model predictive control of a tandem-rotor helicopter. The error is formulated using the matrix Lie group $SE_{2}{(}3{)}$ . A reference trajectory to a target is calculated using a quartic guidance law, leveraging… read more here.
Keywords: control tandem; tandem rotor; control; horizon ... See more keywords