Reconfigurability analysis of multirotor UAVs under actuator faults
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Document typeConference report
Defense date2019
PublisherInstitute of Electrical and Electronics Engineers (IEEE)
Rights accessRestricted access - publisher's policy
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Abstract
This paper presents a reconfigurability analysis for different multirotor structures. The aim is to determine whether the multirotor is able to continue the mission without losing its controllability when faults occur in its actuators. The classical controllability condition is not enough in these systems. Hence two complementary methodologies have been developed to analyse the controllability of the multirotors: Analysis of the Static Reconfiguration Module (ASRM) and Attainable Control Set (ACS).
CitationSanjuan, A.; Nejjari, F.; Sarrate, R. Reconfigurability analysis of multirotor UAVs under actuator faults. A: Conference on Control and Fault Tolerant Systems. "2019 4th Conference on Control and Fault Tolerant Systems (SysTol): proceedings". Institute of Electrical and Electronics Engineers (IEEE), 2019, p. 26-31.
ISBN9781728103815
Publisher versionhttps://ieeexplore.ieee.org/document/8864748
Collections
- Departament d'Enginyeria de Sistemes, Automàtica i Informàtica Industrial - Ponències/Comunicacions de congressos [1.438]
- SIC - Sistemes Intel·ligents de Control - Ponències/Comunicacions de congressos [150]
- SAC - Sistemes Avançats de Control - Ponències/Comunicacions de congressos [550]
- Doctorat en Automàtica, Robòtica i Visió - Ponències/Comunicacions de congressos [135]
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Systol19_Multirotor6mod.pdf![]() | postprint | 381,2Kb | Restricted access |