DocumentCode :
710797
Title :
Decision-support tool for designing small package delivery aerial vehicles (DST-SPDAV)
Author :
Ali, Ashruf ; Ballou, Nathan ; McDougall, Brad ; Valle Ramos, Jorge Luis
fYear :
2015
fDate :
24-24 April 2015
Firstpage :
45
Lastpage :
50
Abstract :
A growing market is the application of multi-rotor vehicles to niche delivery services such as just-in-time spare parts delivery, real-time asset repositioning, rapid food delivery, and remote medical supply delivery. These services are unique in their requirements, meaning there is no single aerial vehicle configuration that is optimal for every scenario. More importantly, these service providers do not have the expertise to design and operate small multi-rotor vehicles that are now feasible due to advances in technology. This is a complex design decision with non-linearities in the design-state-space. This paper presents a decision-support tool to assist small package delivery service providers in configuring the best multi-rotor vehicle for their payload application. The decision-support tool for the design of multi-rotor small package delivery aerial vehicles (SPDAV) takes inputs such as payload, wind, maximum dimension data, price range, and flight profile, and recommends suitable configurations. The algorithm used to generate the design-state-space consists of two separate models of multi-rotor aircraft: (1) a power consumption model and (2) a full dynamic flight model. The power consumption model evaluates the steady-state performance of the battery, motor, and propeller combinations at hover, 80%, and full throttle to determine systems that satisfy the users´ requirements. A dynamic flight model is then applied to these configurations to further account for airframe aerodynamics. A detailed example of the tool for a college campus fast food restaurant is provided.
Keywords :
aerodynamics; aerospace components; autonomous aerial vehicles; design engineering; helicopters; rotors (mechanical); wind; DST-SPDAV; airframe aerodynamics; battery; decision-support tool; design-state-space; flight profile; full dynamic flight model; hover; just-in-time spare parts delivery; maximum dimension data; motor; multirotor aircraft; multirotor small package delivery aerial vehicles design; nonlinearities; payload application; power consumption model; price range; propeller; rapid food delivery; real-time asset repositioning; remote medical supply delivery; service delivery; small package delivery service providers; steady-state performance; users requirements; wind; Atmospheric modeling; Batteries; Mathematical model; Payloads; Propellers; Rotors; Vehicles; Aerodynamics; Dynamic-Model; Multi-Rotor; Power Model; Quadcopter; Tradespace; UAS; UAV;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Systems and Information Engineering Design Symposium (SIEDS), 2015
Conference_Location :
Charlottesville, VA
Print_ISBN :
978-1-4799-1831-7
Type :
conf
DOI :
10.1109/SIEDS.2015.7117009
Filename :
7117009
Link To Document :
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