Required Moment Sets: Enhanced Controllability Analysis for Nonlinear Aircraft Models
Attainable moment sets (AMS) are a powerful method to assess aircraft controllability. However, as attainable moment sets only take into account the achievable moment set of the control effectors, they do not assess the required moment set to fulfill the aircraft mission requirements. This paper pro...
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doaj-d19147b2f2b84fc89dbe0e1dc13db67e2021-04-12T23:03:15ZengMDPI AGApplied Sciences2076-34172021-04-01113456345610.3390/app11083456Required Moment Sets: Enhanced Controllability Analysis for Nonlinear Aircraft ModelsMax Söpper0Jiannan Zhang1Niclas Bähr2Florian Holzapfel3Institute of Flight System Dynamics, Technical University of Munich, 85748 Garching bei München, GermanyInstitute of Flight System Dynamics, Technical University of Munich, 85748 Garching bei München, GermanyInstitute of Flight System Dynamics, Technical University of Munich, 85748 Garching bei München, GermanyInstitute of Flight System Dynamics, Technical University of Munich, 85748 Garching bei München, GermanyAttainable moment sets (AMS) are a powerful method to assess aircraft controllability. However, as attainable moment sets only take into account the achievable moment set of the control effectors, they do not assess the required moment set to fulfill the aircraft mission requirements. This paper proposes to calculate a corresponding required moment set (RMS) which defines a set of moments sufficient for fulfilling aircraft controllability requirements in the mission flight envelope. The paper applies the required moment set approach to a nonlinear simulation model of an electric vertical take off vehicle (eVTOL) transition drone in hover. By comparing the required moment set to the AMS of the aircraft model, moment set margins are derived and used to assess the controllability of the considered aircraft. The results indicate that the combined evaluation directly identifies critical moment channels and margins, which is advantageous when compared to a pure AMS-based evaluation. The proposed approach enables the execution of simulation-based assessments in aircraft design and flight control development. In the early stages of aircraft design, required moment sets can support sizing, positioning and tilting of control effectors (e.g., propulsive elements) to fit the AMS to the actual required force and moment set for the specific system.https://www.mdpi.com/2076-3417/11/8/3456controllabilityeVTOLattainable moment set |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Max Söpper Jiannan Zhang Niclas Bähr Florian Holzapfel |
spellingShingle |
Max Söpper Jiannan Zhang Niclas Bähr Florian Holzapfel Required Moment Sets: Enhanced Controllability Analysis for Nonlinear Aircraft Models Applied Sciences controllability eVTOL attainable moment set |
author_facet |
Max Söpper Jiannan Zhang Niclas Bähr Florian Holzapfel |
author_sort |
Max Söpper |
title |
Required Moment Sets: Enhanced Controllability Analysis for Nonlinear Aircraft Models |
title_short |
Required Moment Sets: Enhanced Controllability Analysis for Nonlinear Aircraft Models |
title_full |
Required Moment Sets: Enhanced Controllability Analysis for Nonlinear Aircraft Models |
title_fullStr |
Required Moment Sets: Enhanced Controllability Analysis for Nonlinear Aircraft Models |
title_full_unstemmed |
Required Moment Sets: Enhanced Controllability Analysis for Nonlinear Aircraft Models |
title_sort |
required moment sets: enhanced controllability analysis for nonlinear aircraft models |
publisher |
MDPI AG |
series |
Applied Sciences |
issn |
2076-3417 |
publishDate |
2021-04-01 |
description |
Attainable moment sets (AMS) are a powerful method to assess aircraft controllability. However, as attainable moment sets only take into account the achievable moment set of the control effectors, they do not assess the required moment set to fulfill the aircraft mission requirements. This paper proposes to calculate a corresponding required moment set (RMS) which defines a set of moments sufficient for fulfilling aircraft controllability requirements in the mission flight envelope. The paper applies the required moment set approach to a nonlinear simulation model of an electric vertical take off vehicle (eVTOL) transition drone in hover. By comparing the required moment set to the AMS of the aircraft model, moment set margins are derived and used to assess the controllability of the considered aircraft. The results indicate that the combined evaluation directly identifies critical moment channels and margins, which is advantageous when compared to a pure AMS-based evaluation. The proposed approach enables the execution of simulation-based assessments in aircraft design and flight control development. In the early stages of aircraft design, required moment sets can support sizing, positioning and tilting of control effectors (e.g., propulsive elements) to fit the AMS to the actual required force and moment set for the specific system. |
topic |
controllability eVTOL attainable moment set |
url |
https://www.mdpi.com/2076-3417/11/8/3456 |
work_keys_str_mv |
AT maxsopper requiredmomentsetsenhancedcontrollabilityanalysisfornonlinearaircraftmodels AT jiannanzhang requiredmomentsetsenhancedcontrollabilityanalysisfornonlinearaircraftmodels AT niclasbahr requiredmomentsetsenhancedcontrollabilityanalysisfornonlinearaircraftmodels AT florianholzapfel requiredmomentsetsenhancedcontrollabilityanalysisfornonlinearaircraftmodels |
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1721529465580814336 |