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- 01H6ZPT3VJK2A4F774BHTBMCCD classification P1.
- 01H6ZPT3VJK2A4F774BHTBMCCD date "2023".
- 01H6ZPT3VJK2A4F774BHTBMCCD language "eng".
- 01H6ZPT3VJK2A4F774BHTBMCCD type conference.
- 01H6ZPT3VJK2A4F774BHTBMCCD hasPart 01H9RHA5D0WCBBJY8H8GEDWE9J.pdf.
- 01H6ZPT3VJK2A4F774BHTBMCCD subject "Technology and Engineering".
- 01H6ZPT3VJK2A4F774BHTBMCCD doi "10.1109/aim46323.2023.10196279".
- 01H6ZPT3VJK2A4F774BHTBMCCD isbn "9781665476331".
- 01H6ZPT3VJK2A4F774BHTBMCCD issn "2159-6255".
- 01H6ZPT3VJK2A4F774BHTBMCCD presentedAt urn:uuid:4e638eab-6225-4da3-995a-263d8ddc1ed2.
- 01H6ZPT3VJK2A4F774BHTBMCCD abstract "In recent years, unmanned aerial systems (UAS) are being utilized for a variety of increasingly complex tasks, including the inspection of offshore installations and the transportation of medical equipment. This has motivated the development of mission-specific dynamic design procedures. The principle of concurrent control and design, also known as co-design, extends the traditional approach of design optimization and trajectory optimization by integrating both into a single treatment. This results in coupled solutions that cannot be achieved using a traditional sequential approach. Studies have demonstrated the effectiveness of combining surrogate-assisted optimization methods, such as Bayesian optimization, with a nested formulation of the co-design problem. In the present work, we extend this approach by simultaneously treating multiple objectives. A reformulation of the Bayesian optimization framework through the use of an alternative acquisition function is fit around a trajectory optimization routine. This results in a novel framework that generates optimized designs that outperform the standard design in various metrics. This allows the designer to select a compromising design based on the system’s application type and confirms the effectiveness of the concurrent design and control procedure. The subsequent methodology is evaluated on the mission-specific design of a fixed-wing unmanned aerial system, with the aim of conducting a survey mission in challenging terrain. To model the dynamics of the aircraft, the differential flatness of the system is utilized.".
- 01H6ZPT3VJK2A4F774BHTBMCCD author 2AF9E22C-F0EE-11E1-A9DE-61C894A0A6B4.
- 01H6ZPT3VJK2A4F774BHTBMCCD author 2DFB9CC2-F0EE-11E1-A9DE-61C894A0A6B4.
- 01H6ZPT3VJK2A4F774BHTBMCCD author F7378570-F0ED-11E1-A9DE-61C894A0A6B4.
- 01H6ZPT3VJK2A4F774BHTBMCCD dateCreated "2023-08-04T07:22:22Z".
- 01H6ZPT3VJK2A4F774BHTBMCCD dateModified "2024-10-29T18:45:35Z".
- 01H6ZPT3VJK2A4F774BHTBMCCD name "Multi-objective co-design for mission-specific development of unmanned aerial systems".
- 01H6ZPT3VJK2A4F774BHTBMCCD pagination urn:uuid:f9fc6f05-09a8-4ec3-8c22-5ca7bab1a75f.
- 01H6ZPT3VJK2A4F774BHTBMCCD publisher urn:uuid:40ab9ff8-baac-4269-a349-34ca320a4bec.
- 01H6ZPT3VJK2A4F774BHTBMCCD sameAs LU-01H6ZPT3VJK2A4F774BHTBMCCD.
- 01H6ZPT3VJK2A4F774BHTBMCCD sourceOrganization urn:uuid:27137605-1ef5-42cb-bfa5-457abf64f754.
- 01H6ZPT3VJK2A4F774BHTBMCCD sourceOrganization urn:uuid:564975e6-d2e2-4220-bb5f-5a5bbf8b38e3.
- 01H6ZPT3VJK2A4F774BHTBMCCD type P1.