Battery health management for small-size rotary-wing electric unmanned aerial vehicles: An efficient approach for constrained computing platforms
Author
dc.contributor.author
Sierra, G.
Author
dc.contributor.author
Orchard, M.
Author
dc.contributor.author
Goebel, K.
Author
dc.contributor.author
Kulkarni, C.
Admission date
dc.date.accessioned
2019-05-31T15:33:52Z
Available date
dc.date.available
2019-05-31T15:33:52Z
Publication date
dc.date.issued
2019
Cita de ítem
dc.identifier.citation
Reliability Engineering and System Safety, Volumen 182, 2019, Pages 166-178
Identifier
dc.identifier.issn
09518320
Identifier
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10.1016/j.ress.2018.04.030
Identifier
dc.identifier.uri
https://repositorio.uchile.cl/handle/2250/169654
Abstract
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This article presents a holistic framework for the design, implementation and experimental validation of Battery Management Systems (BMS) in rotatory-wing Unmanned Aerial Vehicles (UAVs) that allows to accurately (i) estimate the State of Charge (SOC), and (ii) predict the End of Discharge (EOD) time of lithium-polymer batteries in small-size multirotors by using a model-based prognosis architecture that is efficient and feasible to implement in low-cost hardware. The proposed framework includes a simplified battery model that incorporates the electric load dependence, temperature dependence and SOC dependence by using the concept of Artificial Evolution to estimate some of its parameters, along with a novel Outer Feedback Correction Loop (OFCL) during the estimation stage which adjusts the variance of the process noise to diminish bias in Bayesian state estimation and helps to compensate problems associated with incorrect initial conditions in a non-observable dynamic system. Also, it provides an aerodynamic-based characterization of future power consumption profiles. A quadrotor has been used as validation platform. The results of this work will allow making decisions about the flight plan and having enough confidence in those decisions so that the mission objectives can be optimally achieved.