Presented here is a Predictor-Based Model Reference Adaptive Control (PMRAC) architecture for a generic transport aircraft. At its core, this architecture features a three-axis, non-linear, dynamic-inversion controller. Command inputs for this baseline controller are provided by pilot roll-rate, pitch-rate, and sideslip commands. This paper will first thoroughly present the baseline controller followed by a description of the PMRAC adaptive augmentation to this control system. Results are presented via a full-scale, nonlinear simulation of NASA s Generic Transport Model (GTM).
Nonlinear Dynamic Inversion Predictor-Based Model Reference Adaptive Controller for a Generic Transport Model
2010
6 pages
Report
Keine Angabe
Englisch
Predictor-Based Model Reference Adaptive Control
NTRS | 2009
|Predictor-Based Model Reference Adaptive Control
NTRS | 2010
|British Library Conference Proceedings | 2010
|Predictor-Based Model Reference Adaptive Control
AIAA | 2009
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