The doi above is for this specific version of this dataset, which is currently the latest. Newer versions may be published in the future. For a link that will always point to the latest version, please use
doi: 10.4121/1c425f5d-943c-4e9c-8c6b-4e026dba20ca

Pollack, Tijmen (2024): MATLAB/SIMULINK(R) Code and Supporting Data for Assessment of Commonalities between Hybrid INDI-based and PID-based Flight Control Design. Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/1c425f5d-943c-4e9c-8c6b-4e026dba20ca.v1

Dataset

• Aerospace Engineering
• Engineering

Feedback Linearization, Flight Control, INDI Control, PID control, Robust Control

MIT

RefWorks, BibTeX, Reference Manager, Endnote, DataCite, NLM, DC, CFF

by Tijmen Pollack

This dataset contains relevant MATLAB/SIMULINK(R) code and supporting data in relation to CHAPTER 4 of the dissertation 'Advances in Dynamic Inversion- based Flight Control Law Design: Multivariable Analysis and Synthesis of Robust and Multi-Objective Design Solutions' by T.S.C. Pollack (2024) [DOI: 10.4233/uuid:28617ba0-461d-48ef-8437-de2aa41034ea]. It concerns robust synthesis of hybrid Incremental Nonlinear Dynamic Inversion (INDI) based and PID-based control laws against mixed uncertainty. Data is generated using MATLAB's Control System Toolbox routines, such as SYSTUNE. For more information, we refer to the respective thesis chapter / publication.

The following datasets are related:

1) MATLAB/SIMULINK(R) Code and Supporting Data for Analysis of Inversion Strategy on Robustness of IDI-based Control Laws (DOI: https://doi.org/10.4121/1c3b2fe8-15ee-4c93-9de3-9e5dddaca6a0)

2) MATLAB/SIMULINK(R) Code and Supporting Data for Assessment of Commonalities between Hybrid INDI-based and PID-based Flight Control Design (DOI: https://doi.org/10.4121/1c425f5d-943c-4e9c-8c6b-4e026dba20ca)

3) MATLAB/SIMULINK(R) Code and Supporting Data for Design of Multi-objective Incremental Control Allocation-based Flight Control Laws (DOI: https://doi.org/10.4121/b265ae09-64ef-4faf-bd77-d18712c11239)

• 2024-10-08 first online, published, posted

4TU.ResearchData

MATLAB/SIMULINK(R) files

Commonalities between Robust Hybrid Incremental Nonlinear Dynamic Inversion and Proportional-Integral-Derivative Flight Control Law Design

• https://doi.org/10.4233/uuid:28617ba0-461d-48ef-8437-de2aa41034ea

TU Delft, Faculty of Aerospace Engineering, Department of Control and Operations, Section Control & Simulation