This paper presents a framework for attitude command tracking flight controller for a general aviation aircraft using Classical and Incremental Nonlinear Dynamic Inversion approaches. The theoretical background and a framework for attitude tracking flight control framework based on the controllers are presented in this paper. A comparative study of attitude tracking performance of the model dependent Nonlinear Dynamic Inversion Controller and the measurement dependent Incremental Nonlinear Dynamic Inversion Controller for a light aircraft is performed through numerical simulations. Also, Performance evaluation of the Classical and Incremental Nonlinear Dynamic Inversion controllers are carried out under nominal conditions, external disturbances and model uncertainties.
Attitude Tracking Control of a Light Aircraft Using Classical and Incremental Nonlinear Dynamic Inversion Approaches
2021-06-15
1036856 byte
Conference paper
Electronic Resource
English
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