Flight Simulation-Driven Research into Simplified Vehicle Operations for Urban Air Mobility

Chakraborty, I; Comer, A.M.; Bhandari, R; Putra, S.H.; Mishra, A. A.; Auburn University. Department of Aerospace Engineering

doi:10.21949/1528234

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Flight Simulation-Driven Research into Simplified Vehicle Operations for Urban Air Mobility

2023-05-01
By Chakraborty, I ; Comer, A.M. ; Bhandari, R ; ...

[PDF-4.22 MB]

English

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Creators:

Chakraborty, I ; Comer, A.M. ; Bhandari, R ; Putra, S.H. ; Mishra, A. A.

Chakraborty, I ; Comer, A.M. ; Bhandari, R ; Putra, S.H. ; Mishra, A. A. Less -
Corporate Creators:

Auburn University. Department of Aerospace Engineering
Corporate Contributors:

United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center ; United States. Department of Transportation. Federal Aviation Administration. Compliance and Airworthiness Division

United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center ; United States. Department of Transportation. Federal Aviation Administration. Compliance and Airworthiness Division Less -
Subject/TRT Terms:

[+]

Aerodynamic Lift Aircraft Air Travel Handling Qualities Task Elements Lift-Plus-Cruise Mobility Urban Transportation Vehicle Operations VTOL Aircraft
Publication/ Report Number:

DOT/FAA/TC-23/10
DOI:

https://doi.org/10.21949/1528234
Resource Type:

Tech Report
Geographical Coverage:

United States
Edition:

Final Report
Contracting Officer:

McGuire, Robert; Sizoo, David; Schaller, Ross
Corporate Publisher:

United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center
Abstract:

The goal of this project was to study the Simplified Vehicle Operations (SVO) paradigm for vertical takeoff and landing (VTOL) urban air mobility (UAM) aircraft through piloted simulations in two fixed-base flight simulators located at the Vehicle Systems, Dynamics, and Design Laboratory (VSDDL), part of the Department of Aerospace Engineering at Auburn University. A lift-plus-cruise (LPC) aircraft flight simulation model was deployed to two flight simulators, with identical cockpit display elements and core flight control system (FCS) architecture, which was based on the Total Energy Control System (TECS). The simulator setups differed in the design of the pilot inceptors and in the inceptor-to-command mappings.
Format:

PDF
Funding:

692M152140004
Collection(s):

FAA Technical Library
Main Document Checksum:

[+]

urn:sha256:86d4f2bdd9293125669a1683020b1104f291ca47e814ceda2f31ee0837786279
Download URL:

https://rosap.ntl.bts.gov/view/dot/68920/dot_68920_DS1.pdf
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Flight Simulation-Driven Research into Simplified Vehicle Operations for Urban Air Mobility

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