A methodology to integrate reliability into the conceptual design of safety-critical multirotor unmanned aerial vehicles-Reference-Cited by-同舟云学术

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A methodology to integrate reliability into the conceptual design of safety-critical multirotor unmanned aerial vehicles

Published:2022-08 Issue: Volume:127 Page:107681
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Liscouët Jonathan^ORCID,Pollet Félix^ORCID,Jézégou Joël,Budinger Marc,Delbecq Scott,Moschetta Jean-Marc

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference63 articles.

1. Aircraft Design: a Conceptual Approach;Raymer,1989

2. Designing Unmanned Aircraft Systems - a Comprehensive Approach;Gundlach,2014

3. Complete preliminary design methodology for electric multirotor;Gatti;J. Aerosp. Eng.,2017

4. Design methodology for heavy-lift unmanned aerial vehicles with coaxial rotors;Ong,2019

5. Practical Methods for Aircraft and Rotorcraft Flight Control Design: An Optimization-Based Approach;Tischler,2018

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2. Aerodynamic and Aeroacoustic Optimization of UAV Rotor Based on Proper Orthogonal Decomposition Method;Journal of Aerospace Engineering;2024-07

3. Design Optimisation Approach of an Outer Rotor Multiphase PM Actuator for Multirotor Aerial Vehicle Applications;Aerospace;2024-02-13

4. Co-design of a multirotor UAV with robust control considering handling qualities and motor failure;Aerospace Science and Technology;2024-01

5. Design of quadcopter for radiation monitoring in nuclear region;AIP Conference Proceedings;2024

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