Tandem Tilt-Wing Control Law Design using Hybrid Nonlinear Dynamic Inversion

Milz, Daniel and May, Marc Simon and Looye, Gertjan (2026) Tandem Tilt-Wing Control Law Design using Hybrid Nonlinear Dynamic Inversion. Journal of Guidance, Control, and Dynamics, pp. 1-9. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.G009361. ISSN 1533-3884.

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Official URL: https://arc.aiaa.org/doi/10.2514/1.G009361

Item URL in elib:

https://elib.dlr.de/213761/

Document Type:

Article

Title:

Tandem Tilt-Wing Control Law Design using Hybrid Nonlinear Dynamic Inversion

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Milz, Daniel	UNSPECIFIED	https://orcid.org/0000-0001-9704-2036	203717969
May, Marc Simon	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Looye, Gertjan	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

January 2026

Journal or Publication Title:

Journal of Guidance, Control, and Dynamics

Refereed publication:

Yes

Open Access:

Yes

Gold Open Access:

In SCOPUS:

Yes

In ISI Web of Science:

Yes

DOI:

10.2514/1.G009361

Page Range:

pp. 1-9

Publisher:

American Institute of Aeronautics and Astronautics (AIAA)

ISSN:

1533-3884

Status:

Published

Keywords:

Flight Control Tilt-Wing eVTOL Nonlinear Dynamic Inversion

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Aeronautics

HGF - Program Themes:

Components and Systems

DLR - Research area:

Aeronautics

DLR - Program:

L CS - Components and Systems

DLR - Research theme (Project):

L - Aircraft Systems

Location:

Oberpfaffenhofen

Institutes and Institutions:

Institute of Flight Systems > Flight Control and Simulation
Institute of Aeroelasticity > Control of Aeroelastic Systems

Deposited By:

Milz, Daniel

Deposited On:

27 Jan 2026 11:55

Last Modified:

11 Feb 2026 08:38

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