Analysis and implementation of a winged-airship for micro transport and test platform

Chin E. Lin; Shih Che Hung; Kuo Ming Lee

Analysis and implementation of a winged-airship for micro transport and test platform

Chin E. Lin, Shih Che Hung, Kuo Ming Lee

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Abstract

Micro transport might contribute to metropolitan services for micro delivery. However, vehicle performance may determine the overall value of this idea. Vehicle design with safety, reliability and stability is studied. The winged-airship is proposed with an idea to adhere a pair of wings in the conventional airship to offer substantial lift, increase wind resistance, and create a natural stability under normal flight condition. Vehicle specifications are considered and designed, and prototype fabrication is implemented. With limited constraints, the design process for the winged-airship is carried out with feasibility analysis and numerical simulation, in order to establish a feasible solution for system fabrication. The experiment result is repeatedly examined by simulation result with modifications.

Original language	English
Title of host publication	AIAA Guidance, Navigation, and Control Conference and Exhibit
Publication status	Published - 2001 Dec 1
Event	AIAA Guidance, Navigation, and Control Conference and Exhibit 2001 - Montreal, QC, Canada Duration: 2001 Aug 6 → 2001 Aug 9

Publication series

Name	AIAA Guidance, Navigation, and Control Conference and Exhibit

Other

Other	AIAA Guidance, Navigation, and Control Conference and Exhibit 2001
Country	Canada
City	Montreal, QC
Period	01-08-06 → 01-08-09

All Science Journal Classification (ASJC) codes

Aerospace Engineering
Control and Systems Engineering
Electrical and Electronic Engineering

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title = "Analysis and implementation of a winged-airship for micro transport and test platform",

abstract = "Micro transport might contribute to metropolitan services for micro delivery. However, vehicle performance may determine the overall value of this idea. Vehicle design with safety, reliability and stability is studied. The winged-airship is proposed with an idea to adhere a pair of wings in the conventional airship to offer substantial lift, increase wind resistance, and create a natural stability under normal flight condition. Vehicle specifications are considered and designed, and prototype fabrication is implemented. With limited constraints, the design process for the winged-airship is carried out with feasibility analysis and numerical simulation, in order to establish a feasible solution for system fabrication. The experiment result is repeatedly examined by simulation result with modifications.",

author = "Lin, {Chin E.} and Hung, {Shih Che} and Lee, {Kuo Ming}",

year = "2001",

month = dec,

day = "1",

language = "English",

isbn = "9781563479786",

series = "AIAA Guidance, Navigation, and Control Conference and Exhibit",

booktitle = "AIAA Guidance, Navigation, and Control Conference and Exhibit",

note = "AIAA Guidance, Navigation, and Control Conference and Exhibit 2001 ; Conference date: 06-08-2001 Through 09-08-2001",

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T1 - Analysis and implementation of a winged-airship for micro transport and test platform

AU - Lin, Chin E.

AU - Hung, Shih Che

AU - Lee, Kuo Ming

PY - 2001/12/1

Y1 - 2001/12/1

N2 - Micro transport might contribute to metropolitan services for micro delivery. However, vehicle performance may determine the overall value of this idea. Vehicle design with safety, reliability and stability is studied. The winged-airship is proposed with an idea to adhere a pair of wings in the conventional airship to offer substantial lift, increase wind resistance, and create a natural stability under normal flight condition. Vehicle specifications are considered and designed, and prototype fabrication is implemented. With limited constraints, the design process for the winged-airship is carried out with feasibility analysis and numerical simulation, in order to establish a feasible solution for system fabrication. The experiment result is repeatedly examined by simulation result with modifications.

AB - Micro transport might contribute to metropolitan services for micro delivery. However, vehicle performance may determine the overall value of this idea. Vehicle design with safety, reliability and stability is studied. The winged-airship is proposed with an idea to adhere a pair of wings in the conventional airship to offer substantial lift, increase wind resistance, and create a natural stability under normal flight condition. Vehicle specifications are considered and designed, and prototype fabrication is implemented. With limited constraints, the design process for the winged-airship is carried out with feasibility analysis and numerical simulation, in order to establish a feasible solution for system fabrication. The experiment result is repeatedly examined by simulation result with modifications.

UR - http://www.scopus.com/inward/record.url?scp=84894431027&partnerID=8YFLogxK

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M3 - Conference contribution

AN - SCOPUS:84894431027

SN - 9781563479786

T3 - AIAA Guidance, Navigation, and Control Conference and Exhibit

BT - AIAA Guidance, Navigation, and Control Conference and Exhibit

T2 - AIAA Guidance, Navigation, and Control Conference and Exhibit 2001

Y2 - 6 August 2001 through 9 August 2001

ER -

Analysis and implementation of a winged-airship for micro transport and test platform

Abstract

Publication series

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All Science Journal Classification (ASJC) codes

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