Experimental evaluation of multi-rotor UAV operation under icing conditions

Sihong Yan, Tomas Opazo, Jose Palacios, Jacob Willem Langelaan, Louis David Germain

Research output: Contribution to journalConference article

1 Citation (Scopus)

Abstract

Unmanned aerial vehicles (UAV) with multi-rotor configurations have become a popular platform for aerial surveillance and and are forecast for use in delivery of packages. During these missions, UAVs can be exposed to icing conditions. In this paper, two icing experiments on representative UAV configurations are discussed. The object of this paper is to investigate the effects of ice accretion on the operation of a UAV. The first experiment is to measure degradation in thrust and increase in power requirements of a co-axial rotor configuration in an icing wind tunnel. The second experimental set-up tested a commercial UAV (DJI Mavic Pro) in a forward flight regime in an artificial icing environment. These co-axial UAV rotors are controlled by two algorithms. The first algorithm keeps a constant rpm during 60 seconds in an icing cloud. The second algorithm maintains thrust until ice shed from rotors. In addition, a DJI Mavic Pro icing flight test was conducted inside an icing chamber. Both experiments demonstrate that ice accretion on UAV rotors can lead to an intimidating deficit in thrust and abrupt increase in power consumption that could result in catastrophic failure. When rpm is fixed, increase in power and decrease in thrust are linearly correlated with icing time. When thrust is constant, rpm and power could be modeled as a linear function of time before ice sheds. Power change rates under varying icing conditions were compared and discussed. In addition, ice shedding events were observed in the wind tunnel test. A shedding event could result in abrupt change in thrust and power affecting the capability of the motor control algorithm to operate. In the DJI icing flight test, motor current exceeded the current safety limit of the motor within 30 seconds of ice exposure. The motor coils heated during the ice accretion process melting the insulation on wires. The test confirmed the almost immediate damage to small UAV (under 50 Kg.) motors and batteries during icing process.

Original languageEnglish (US)
JournalAnnual Forum Proceedings - AHS International
Volume2018-May
StatePublished - Jan 1 2018
Event74th American Helicopter Society International Annual Forum and Technology Display 2018: The Future of Vertical Flight - Phoenix, United States
Duration: May 14 2018May 17 2018

Fingerprint

Unmanned aerial vehicles (UAV)
Ice
Rotors
Wind tunnels
Experiments
Insulation
Melting
Electric power utilization
Wire
Antennas
Degradation

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

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title = "Experimental evaluation of multi-rotor UAV operation under icing conditions",
abstract = "Unmanned aerial vehicles (UAV) with multi-rotor configurations have become a popular platform for aerial surveillance and and are forecast for use in delivery of packages. During these missions, UAVs can be exposed to icing conditions. In this paper, two icing experiments on representative UAV configurations are discussed. The object of this paper is to investigate the effects of ice accretion on the operation of a UAV. The first experiment is to measure degradation in thrust and increase in power requirements of a co-axial rotor configuration in an icing wind tunnel. The second experimental set-up tested a commercial UAV (DJI Mavic Pro) in a forward flight regime in an artificial icing environment. These co-axial UAV rotors are controlled by two algorithms. The first algorithm keeps a constant rpm during 60 seconds in an icing cloud. The second algorithm maintains thrust until ice shed from rotors. In addition, a DJI Mavic Pro icing flight test was conducted inside an icing chamber. Both experiments demonstrate that ice accretion on UAV rotors can lead to an intimidating deficit in thrust and abrupt increase in power consumption that could result in catastrophic failure. When rpm is fixed, increase in power and decrease in thrust are linearly correlated with icing time. When thrust is constant, rpm and power could be modeled as a linear function of time before ice sheds. Power change rates under varying icing conditions were compared and discussed. In addition, ice shedding events were observed in the wind tunnel test. A shedding event could result in abrupt change in thrust and power affecting the capability of the motor control algorithm to operate. In the DJI icing flight test, motor current exceeded the current safety limit of the motor within 30 seconds of ice exposure. The motor coils heated during the ice accretion process melting the insulation on wires. The test confirmed the almost immediate damage to small UAV (under 50 Kg.) motors and batteries during icing process.",
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Experimental evaluation of multi-rotor UAV operation under icing conditions. / Yan, Sihong; Opazo, Tomas; Palacios, Jose; Langelaan, Jacob Willem; Germain, Louis David.

In: Annual Forum Proceedings - AHS International, Vol. 2018-May, 01.01.2018.

Research output: Contribution to journalConference article

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AU - Yan, Sihong

AU - Opazo, Tomas

AU - Palacios, Jose

AU - Langelaan, Jacob Willem

AU - Germain, Louis David

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N2 - Unmanned aerial vehicles (UAV) with multi-rotor configurations have become a popular platform for aerial surveillance and and are forecast for use in delivery of packages. During these missions, UAVs can be exposed to icing conditions. In this paper, two icing experiments on representative UAV configurations are discussed. The object of this paper is to investigate the effects of ice accretion on the operation of a UAV. The first experiment is to measure degradation in thrust and increase in power requirements of a co-axial rotor configuration in an icing wind tunnel. The second experimental set-up tested a commercial UAV (DJI Mavic Pro) in a forward flight regime in an artificial icing environment. These co-axial UAV rotors are controlled by two algorithms. The first algorithm keeps a constant rpm during 60 seconds in an icing cloud. The second algorithm maintains thrust until ice shed from rotors. In addition, a DJI Mavic Pro icing flight test was conducted inside an icing chamber. Both experiments demonstrate that ice accretion on UAV rotors can lead to an intimidating deficit in thrust and abrupt increase in power consumption that could result in catastrophic failure. When rpm is fixed, increase in power and decrease in thrust are linearly correlated with icing time. When thrust is constant, rpm and power could be modeled as a linear function of time before ice sheds. Power change rates under varying icing conditions were compared and discussed. In addition, ice shedding events were observed in the wind tunnel test. A shedding event could result in abrupt change in thrust and power affecting the capability of the motor control algorithm to operate. In the DJI icing flight test, motor current exceeded the current safety limit of the motor within 30 seconds of ice exposure. The motor coils heated during the ice accretion process melting the insulation on wires. The test confirmed the almost immediate damage to small UAV (under 50 Kg.) motors and batteries during icing process.

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M3 - Conference article

VL - 2018-May

JO - Annual Forum Proceedings - AHS International

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