PI(D) tuning for Flight Control Systems via Incremental Nonlinear Dynamic Inversion

Conference Paper (2017)
Author(s)

P. Acquatella (Deutsches Zentrum für Luft- und Raumfahrt (DLR))

Wim van Ekeren (Deutsches Zentrum für Luft- und Raumfahrt (DLR))

Qi Ping Chu (TU Delft - Control & Simulation)

Research Group
Control & Simulation
DOI related publication
https://doi.org/10.1016/j.ifacol.2017.08.1265
More Info
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Publication Year
2017
Language
English
Research Group
Control & Simulation
Volume number
50
Pages (from-to)
8175-8180

Abstract

Previous results reported in the robotics literature show the relationship between time-delay control (TDC) and proportional-integral-derivative control (PID). In this paper, we show that incremental nonlinear dynamic inversion (INDI) — more familiar in the aerospace community — are in fact equivalent to TDC. This leads to a meaningful and systematic method for PI(D)-control tuning of robust nonlinear flight control systems via INDI. We considered a reformulation of the plant dynamics inversion which removes effector blending models from the resulting control law, resulting in robust model-free control laws like PI(D)-control.

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