James D. Walker, F. M. Heim, B. Surampudi, Pablo Bueno, Alexander Carpenter, S. Chocron, Jon T. Cutshall, Richard Lammons, Theodore Bapty, Brian Swenson, Sydney Whittington
{"title":"A Flight Dynamics Model for Exploring the Distributed Electrical eVTOL Cyber Physical Design Space","authors":"James D. Walker, F. M. Heim, B. Surampudi, Pablo Bueno, Alexander Carpenter, S. Chocron, Jon T. Cutshall, Richard Lammons, Theodore Bapty, Brian Swenson, Sydney Whittington","doi":"10.1109/DESTION56136.2022.00008","DOIUrl":null,"url":null,"abstract":"As part of DARPA’s Symbiotic Design for Cyber Physical Systems program, software tools were developed for a UAV and air taxi eVTOL design challenge. These included the development of a corpus of parts, an assembly technique, and then a 6-degree-of-freedom flight dynamics model with an autopilot based on trim states and a linear quadratic regulator to fly the assembled air vehicle. This paper describes the flight dynamics model and autopilot and controls in some detail. It also presents examples of parts, designs and performance.","PeriodicalId":273969,"journal":{"name":"2022 IEEE Workshop on Design Automation for CPS and IoT (DESTION)","volume":"118 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2022-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"5","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2022 IEEE Workshop on Design Automation for CPS and IoT (DESTION)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/DESTION56136.2022.00008","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 5
Abstract
As part of DARPA’s Symbiotic Design for Cyber Physical Systems program, software tools were developed for a UAV and air taxi eVTOL design challenge. These included the development of a corpus of parts, an assembly technique, and then a 6-degree-of-freedom flight dynamics model with an autopilot based on trim states and a linear quadratic regulator to fly the assembled air vehicle. This paper describes the flight dynamics model and autopilot and controls in some detail. It also presents examples of parts, designs and performance.