Tilt-Wing Control Design for a Unified Control Concept

von Milz, Daniel
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Guidance, navigation, and control ; Volume 4 of 4 (2022)

DESIGN AND EVALUATION OF ADVANCED INTELLIGENT FLIGHT CONTROLLERS

von Milz, Daniel M.
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Intelligent systems ; Volume 2 of 2 (2020)

Lateral Guidance Control Using Information of Preceding Wheel Pairs

von Grether, Gustav
Veröffentlicht in Symposium on Dynamics of Vehicles on Roads and Tracks (26. : 2019 : Göteborg) Advances in dynamics of vehicles on roads and tracks ; Set 1 (2020)

ANALYSIS OF AUTOMATIC CONTROL FUNCTION EFFECTS ON VERTICAL TAIL PLANE CRITICAL LOAD CONDITIONS

von Kier, Thiemo M.
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Intelligent systems ; Volume 2 of 2 (2020)

Dynamic Modeling and Analysis of Tilt-Wing Electric Vertical Take-Off and Landing Vehicles

von May, Marc S.
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Unique and transformational flight systems (2022)

AUTOMATIC LANDING DESIGN FOR OVERWEIGHT TRANSPORT AIRCRAFT WITH EXPLICIT FLARE CONTROLLER AND INCREMENTAL

von Cárdenas, José Ignacio De Alvear
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Intelligent systems ; Volume 2 of 3 (2021)

Semi-Empirical Aerodynamic Modeling Approach for Tandem Tilt-Wing eVTOL Control Design Applications

von May, Marc S.
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Aircraft design ; Volume 2 of 2 (2023)

Robust performance analysis for gust loads computation

von Knoblach, Andreas Joachim
Veröffentlicht 2015

Semi-Empirical Aerodynamic Modeling Approach for Tandem Tilt-Wing eVTOL Control Design Applications

von May, Marc S.
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Unique and transformational flight systems (2023)

REINFORCEMENT LEARNING BASED ONLINE ADAPTIVE FLIGHT CONTROL FOR THE CESSNA CITATION II(PH-LAB) AIRCRAFT

von Konatala, Ramesh
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Intelligent systems ; Volume 2 of 3 (2021)

Design and Flight Testing of Flight Control Laws Integrating Incremental Nonlinear Dynamic Inversion and Servo Current Control

von Pollack, Tijmen
Veröffentlicht in AIAA SciTech Forum and Exposition (2019 : San Diego, Calif.) Intelligent systems ; Volume 1 of 2 (2019)

Design and Flight Testing of Incremental Backstepping based Control Laws with Angular Accelerometer Feedback

von Keijzer, Twan
Veröffentlicht in AIAA SciTech Forum and Exposition (2019 : San Diego, Calif.) Intelligent systems ; Volume 1 of 2 (2019)

AIRCRAFT MISSION SIMULATION FRAMEWORK FOR LOADS ANALYSIS

von Schulz, Simon
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Intelligent systems ; Volume 2 of 2 (2020)

OMAHA - Overall management architecture for health analysis : Abschlussbericht OMAHA

von Windelberg, Jens
Veröffentlicht 2017

FLIGHT TESTING A LINEAR PARAMETER VARYING CONTROL LAW ON A PASSENGER AIRCRAFT

von Weiser, Christian
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Intelligent systems ; Volume 2 of 2 (2020)

Advances in aerospace guidance, navigation and control : selected papers of the second CEAS Specialist Conference on Guidance, Navigation and Control ; [CEAS EuroGNC 2013 ; in De...

Veröffentlicht 2013

RESULTS OF AN AEROELASTICALLY TAILORED WING ON THE FLEXOP DEMONSTRATOR AIRCRAFT

von Roessler, Christian
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Atmospheric flight mechanics ; Volume 2 of 2 (2020)

ACTIVE FLUTTER MITIGATION TESTING ON THE FLEXOP DEMONSTRATOR AIRCRAFT

von Takarics, Béla
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Atmospheric flight mechanics ; Volume 2 of 2 (2020)