UAM Disturbance Rejection in Conceptual Design, Phase I

Metadata Updated: February 28, 2019

Complex and often violent urban wind environments pose a significant challenge to the safety and ride quality for vehicles intended for the Urban Air Mobility (UAM) market. UAM aircraft concepts must have control authority, turbulence rejection, and ride comfort as figures of merit at the forefront of the configuration selection process.[HTML_REMOVED]However, the evaluation of handling qualities has traditionally been[HTML_REMOVED]late in the design process when most of a vehicle[HTML_REMOVED]s characteristics are established. Advanced design methods in early conceptual design are just recently adopting the use of physics-based aircraft dynamics models to identify handling quality metrics and educate the configuration down selection process. Attempts to extend those tools into unique VTOL configurations designed for the UAM market are not ubiquitous due to the increased complexity and diversity of VTOL concepts.

Empirical Systems Aerospace, Inc., (ESAero) will develop[HTML_REMOVED]a quantitative ride quality assessment methodology and accompanying tool suite to enable the analysis and down-selection of eVTOL configurations during the conceptual design process. ESAero will leverage previous development of 6DoF dynamics simulations of vehicles with distributed electric propulsion (DEP) control authority to integrate handling qualities into the design and configuration process where system level changes are least expensive. Physics-based models in ESAero[HTML_REMOVED]s Propulsion Airframe iNTegration for Hybrid Electric Research (PANTHER) tool suite will be extended to scalable dynamics models for the latest eVTOL propulsion technologies such as electric ducted fans (EDF) and small, distributed propellers. ESAero[HTML_REMOVED]s recent expansion of OpenVSP/VSPAERO to characterize[HTML_REMOVED]handling qualities will be utilized in the creation of the dynamics simulations.[HTML_REMOVED] By leveraging OpenVSP, PANTHER, and physics based 6DoF simulation, this effort will enable rapid evaluation of handling qualities[HTML_REMOVED]at the forefront of the conceptual design process.

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Public: This dataset is intended for public access and use. License: U.S. Government Work

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Metadata Created Date February 28, 2019
Metadata Updated Date February 28, 2019

Metadata Source

Harvested from NASA Data.json

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Resource Type Dataset
Metadata Created Date February 28, 2019
Metadata Updated Date February 28, 2019
Publisher Space Technology Mission Directorate
Unique Identifier TECHPORT_94780
Maintainer Email
Public Access Level public
Bureau Code 026:00
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Metadata Catalog ID
Schema Version
Catalog Describedby
Harvest Object Id 86962d5b-8238-4d0e-b979-049120efadb2
Harvest Source Id 39e4ad2a-47ca-4507-8258-852babd0fd99
Harvest Source Title NASA Data.json
Data First Published 2019-01-01
Homepage URL
Data Last Modified 2018-09-07
Program Code 026:027
Source Datajson Identifier True
Source Hash e5fb225d7d742cf7e5aa9c65f0b89d0c1141dc23
Source Schema Version 1.1

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