Gomes dos Santos, Willer und Rocco, Evandro Marconi und Boge, Toralf und Benninghoff, Heike und Rems, Florian (2015) A novel solution for the spacecraft mixed actuators problem based on a multiobjective optimization method. In: 25th International Symposium on Space Flight Dynamics, 25. International Symposium on Space Flight Dynamics, 2015-10-19 - 2015-10-23, München, Deutschland.
![]() |
PDF
16MB |
Kurzfassung
In this paper, a novel solution for the mixed actuators problem is proposed. This approach uses a multiobjective optimization technique for commanding a group of actuators (thrusters, reaction wheels and magnetic torqrods) simultaneously optimizing a set of objective functions. The multiobjective problem is formulated using combinatorial combinations of the control signal for composing the decision space. The proposed model, called Actuator Multiobjective Command Method (AMCM), is included in a complete guidance, navigation and control loop applied to the final approach rendezvous scenario. Its performance, compared to different actuators configurations, has been evaluated in numerical simulations. In addition, AMCM has been integrated and tested in the hardware-in-the-loop rendezvous and docking simulator of the German Aerospace Center. Results have indicated effectiveness and robustness in both purely numerical and real-time simulations.
elib-URL des Eintrags: | https://elib.dlr.de/100169/ | ||||||||||||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||
Titel: | A novel solution for the spacecraft mixed actuators problem based on a multiobjective optimization method | ||||||||||||||||||||||||
Autoren: |
| ||||||||||||||||||||||||
Datum: | Oktober 2015 | ||||||||||||||||||||||||
Erschienen in: | 25th International Symposium on Space Flight Dynamics | ||||||||||||||||||||||||
Referierte Publikation: | Nein | ||||||||||||||||||||||||
Open Access: | Ja | ||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||
Band: | 25 | ||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||
Stichwörter: | Mixed Actuators Problems, Multiobjective Optimization, Final Approach Rendezvous | ||||||||||||||||||||||||
Veranstaltungstitel: | International Symposium on Space Flight Dynamics | ||||||||||||||||||||||||
Veranstaltungsort: | München, Deutschland | ||||||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||
Veranstaltungsbeginn: | 19 Oktober 2015 | ||||||||||||||||||||||||
Veranstaltungsende: | 23 Oktober 2015 | ||||||||||||||||||||||||
Veranstalter : | DLR Raumflugbetrieb und Astronautentraining, Raumflugtechnologie, Oberpfaffenhofen | ||||||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||
HGF - Programm: | Raumfahrt | ||||||||||||||||||||||||
HGF - Programmthema: | Technik für Raumfahrtsysteme | ||||||||||||||||||||||||
DLR - Schwerpunkt: | Raumfahrt | ||||||||||||||||||||||||
DLR - Forschungsgebiet: | R SY - Technik für Raumfahrtsysteme | ||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | R - Projekt OOS-E2E (alt) | ||||||||||||||||||||||||
Standort: | Oberpfaffenhofen | ||||||||||||||||||||||||
Institute & Einrichtungen: | Raumflugbetrieb und Astronautentraining > Raumflugtechnologie | ||||||||||||||||||||||||
Hinterlegt von: | Frei, Heike | ||||||||||||||||||||||||
Hinterlegt am: | 07 Dez 2015 09:34 | ||||||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 20:05 |
Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags