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Pusch, Manuel (2017) Allocation of Distributed Flaps for Gust Load Alleviation. 1st Conference on Control Technology and Application, 27.8.-30.8.2017, Waimea, HI, USA.
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Kurzfassung
Increasing the number and functionality of control surfaces provides great potential to improve aircraft performance. This, however, complicates the design of the control allocation system commonly used for flight control. A novel method for linear control allocation is presented which allows considering an arbitrary number of frequency dependent control objectives. The method systematically identifies principal control input directions for predefined performance channels by means of a balancing state space transformation. The effectiveness of the method is proven by designing a gust load alleviation system for a flexible aircraft with distributed trailing edge flaps.
| elib-URL des Eintrags: | https://elib.dlr.de/114164/ | ||||||||
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| Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||
| Titel: | Allocation of Distributed Flaps for Gust Load Alleviation | ||||||||
| Autoren: |
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| Datum: | August 2017 | ||||||||
| Referierte Publikation: | Ja | ||||||||
| Open Access: | Ja | ||||||||
| Gold Open Access: | Nein | ||||||||
| In SCOPUS: | Nein | ||||||||
| In ISI Web of Science: | Nein | ||||||||
| Status: | veröffentlicht | ||||||||
| Stichwörter: | Control Allocation, Gust Load Alleviation, Flexible Aircraft, Aeroelasticity, Balanced Truncation | ||||||||
| Veranstaltungstitel: | 1st Conference on Control Technology and Application | ||||||||
| Veranstaltungsort: | Waimea, HI, USA | ||||||||
| Veranstaltungsart: | internationale Konferenz | ||||||||
| Veranstalter : | IEEE | ||||||||
| HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||
| HGF - Programm: | Raumfahrt | ||||||||
| HGF - Programmthema: | keine Zuordnung | ||||||||
| DLR - Schwerpunkt: | Raumfahrt | ||||||||
| DLR - Forschungsgebiet: | R - keine Zuordnung | ||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | R - keine Zuordnung | ||||||||
| Standort: | Oberpfaffenhofen | ||||||||
| Institute & Einrichtungen: | Institut für Systemdynamik und Regelungstechnik > Flugzeug-Systemdynamik | ||||||||
| Hinterlegt von: | Pusch, Manuel | ||||||||
| Hinterlegt am: | 25 Sep 2017 16:55 | ||||||||
| Letzte Änderung: | 31 Jul 2019 20:11 |
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- Allocation of Distributed Flaps for Gust Load Alleviation. (deposited 25 Sep 2017 16:55) [Gegenwärtig angezeigt]
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