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Decision-making for unmanned aerial vehicle operation in icing conditions
- Source :
- CEAS Aeronautical Journal, 7(4)
- Publication Year :
- 2016
- Publisher :
- Springer Verlag, 2016.
-
Abstract
- With the increased use of unmanned aerial systems (UAS) for civil and commercial applications, there is a strong demand for new regulations and technology that will eventually permit for the integration of UAS in unsegregated airspace. This requires new technology to ensure sufficient safety and a smooth integration process. The absence of a pilot on board a vehicle introduces new problems that do not arise in manned flight. One challenging and safety-critical issue is flight in known icing conditions. Whereas in manned flight, dealing with icing is left to the pilot and his appraisal of the situation at hand; in unmanned flight, this is no longer an option and new solutions are required. To address this, an icing-related decision-making system (IRDMS) is proposed. The system quantifies in-flight icing based on changes in aircraft performance and measurements of environmental properties, and evaluates what the effects on the aircraft are. Based on this, it determines whether the aircraft can proceed, and whether and which available icing protection systems should be activated. In this way, advice on an appropriate response is given to the operator on the ground, to ensure safe continuation of the flight and avoid possible accidents.
- Subjects :
- 020301 aerospace & aeronautics
0209 industrial biotechnology
Engineering
Process (engineering)
business.industry
Unmanned aerial system
Aerospace Engineering
Transportation
ComputerApplications_COMPUTERSINOTHERSYSTEMS
02 engineering and technology
Protection system
Aircraft icing
Flight simulator
Drone
On board
020901 industrial engineering & automation
Icing conditions
0203 mechanical engineering
Aeronautics
Ice detection
business
Icing
Decision-making
Subjects
Details
- ISSN :
- 18695582
- Database :
- OpenAIRE
- Journal :
- CEAS Aeronautical Journal, 7(4)
- Accession number :
- edsair.doi.dedup.....9d00294057a66fc986e154fc816edd0d