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Mr. Christoph Stuckmann
MACCON

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Research Keywords & Expertise

0 Motor and Drive design
0 motor
0 Motor and Electrical appliances
0 Motor activity
0 Motor and drive control

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Short Biography

Education: Graduate Engineer (university) / Electrical Engineering Technical University of Dortmund Skills: Management: Senior development engineer at MACCON Languages: Deutsch / English Professional Experience: Technical University of Dortmund/ Chair of Electrical Machines 2003-2006: research assistant at University of Dortmund - Development of an high temperature Electrical Motor for a hybrid car concept - Teaching in science of Electrical Machines - Different Developments in industrial Projects Siemens AG/ Automation and Drives/ Large Drives Industry/ R & D Engineer 2006-2008: Development of Electrical Motors with integrated cooling pipes in the Lamination for synchronous/ asynchronous industrial Motors with management position Current Position Main topic / development project / task areas: - Development and design of special motors in MACCON GmbH - Development of special electric motors in various space projects - Various motor drive developments in the e-mobility sector - Further development of various projects for industrial applications and in the field of research - Software sales and support of software products

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Journal article
Published: 25 July 2021 in Actuators
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Electro-mechanical actuators (EMAs) are a primary actuation technology for unmanned aerial vehicles (UAVs). Intensive research has been conducted for designing and evaluating fault-tolerant EMAs for flight controls of UAVs to ensure their compliance with new airworthiness requirements for safe operation over civilian zones. The state-of-the-art research involves several fault-tolerant architectures for EMAs based on parallel electric motors or a single motor with internal fault-tolerant features. In this study, a fault-tolerant architecture is introduced, comprised of two serial electric motors driven by two isolated controllers and a health monitoring system. The procedures of developing various fault-tolerant features are discussed with a deep focus on designing health monitoring functions and evaluating their influence on the overall actuator stability and availability. This work has been conducted and evaluated based on operational data for ALAADy: a heavy gyrocopter-type UAV at DLR (German Aerospace Center).

ACS Style

Mohamed Ismail; Simon Wiedemann; Colin Bosch; Christoph Stuckmann. Design and Evaluation of Fault-Tolerant Electro-Mechanical Actuators for Flight Controls of Unmanned Aerial Vehicles. Actuators 2021, 10, 175 .

AMA Style

Mohamed Ismail, Simon Wiedemann, Colin Bosch, Christoph Stuckmann. Design and Evaluation of Fault-Tolerant Electro-Mechanical Actuators for Flight Controls of Unmanned Aerial Vehicles. Actuators. 2021; 10 (8):175.

Chicago/Turabian Style

Mohamed Ismail; Simon Wiedemann; Colin Bosch; Christoph Stuckmann. 2021. "Design and Evaluation of Fault-Tolerant Electro-Mechanical Actuators for Flight Controls of Unmanned Aerial Vehicles." Actuators 10, no. 8: 175.