Electrical drivetrain of the small airplane and mutual interaction of this drivetrain

Pazdera, Ivo; Procházka, Petr; Cervinka, Dalibor; Klima, Bohumil

doi:10.1109/iecon.2013.6699881

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2014

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“…Acceleration a x is calculated from Eqs. (4) and (5), and all the parameters of the experiment are the same as that of the simulation.…”

Section: A Experimental Setupmentioning

confidence: 99%

Range extension control system for electric airplane with multiple motors by optimization of thrust distribution considering propellers efficiency

Konishi

Fujimoto

Kobayashi

et al. 2014

IECON 2014 - 40th Annual Conference of the IEEE Industrial Electronics Society

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In the recent years, attention has been gathered in the research field of electric airplanes (EAs), which have electric motors as a power source. EAs have many advantages including low environmental impact and safety. The flight range per charge, however, is shorter than that of conventional airplanes. This paper proposes a range extention control system (RECS) which extends the flight range of EAs by control. It is shown that the power consumption can be minimized by optimizing thrust distribution on multiple propellers with different properties. The effectiveness of the proposed method is verified by simulations and experiments.

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“…Acceleration a x is calculated from Eqs. (4) and (5), and all the parameters of the experiment are the same as that of the simulation.…”

Section: A Experimental Setupmentioning

confidence: 99%

Range extension control system for electric airplane with multiple motors by optimization of thrust distribution considering propellers efficiency

Konishi

Fujimoto

Kobayashi

et al. 2014

IECON 2014 - 40th Annual Conference of the IEEE Industrial Electronics Society

View full text Add to dashboard Cite

show abstract

Electrical drivetrain of the small airplane and mutual interaction of this drivetrain

Cited by 1 publication

References 7 publications

Range extension control system for electric airplane with multiple motors by optimization of thrust distribution considering propellers efficiency

Range extension control system for electric airplane with multiple motors by optimization of thrust distribution considering propellers efficiency

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