Consideration of control effector dynamics and saturations in an extended indi approach

Stefan Raab, Jiannan Zhang, Pranav Bhardwaj, Florian Holzapfel

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

18 Scopus citations

Abstract

This paper proposes an extension of the conventional Incremental Nonlinear Dynamic Inversion (INDI) approach, which enhances the inherent advantages by consideration of control effector dynamics and saturations. The inversion law is derived from a continuous system point of view and presents the resulting system in an intuitive way. First and second order control effectors including absolute and rate saturations can be taken into account in the proposed approach and enable a physically transparent way of designing pseudo control loop and outer loops. The proposed approach is first derived in general and then applied to a simple example system. Lastly, results of a real test flight of the proposed algorithm on a VTOL transition drone are presented. The proposed extension reduces cross couplings in different channels in the presence of control effectors with dissimilar bandwidhts and system orders, and furthermore enables an intuitive way of outer loop gain design. In case of redundant control effectors or "over-actuation", the control effectors are utilized depending on their bandwidth. The algorithm gives promising results and is focus of future research.

Original languageEnglish
Title of host publicationAIAA Aviation 2019 Forum
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
Pages1-13
Number of pages13
ISBN (Print)9781624105890
DOIs
StatePublished - 2019
EventAIAA Aviation 2019 Forum - Dallas, United States
Duration: 17 Jun 201921 Jun 2019

Publication series

NameAIAA Aviation 2019 Forum

Conference

ConferenceAIAA Aviation 2019 Forum
Country/TerritoryUnited States
CityDallas
Period17/06/1921/06/19

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