Flight Control Design using Incremental Nonlinear Dynamic Inversion with Fixed-lag Smoothing Estimation

Volume: 21, Issue: 4, Pages: 1047 - 1058
Published: Apr 14, 2020
Abstract
In this study, a flight control design strategy based on incremental nonlinear dynamic inversion (INDI) and smoothing algorithm is presented. The INDI is an enhanced version of the nonlinear dynamic inversion technique with a better robust performance. It reduces the aircraft model dependence via the feedback information of the state derivative, that is, angular acceleration for the aircraft attitude motion (or angular velocity related to the...
Paper Details
Title
Flight Control Design using Incremental Nonlinear Dynamic Inversion with Fixed-lag Smoothing Estimation
Published Date
Apr 14, 2020
Volume
21
Issue
4
Pages
1047 - 1058
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