elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Impressum | Datenschutz | Kontakt | English
Schriftgröße: [-] Text [+]

SPARTAN: A Novel Pseudospectral Algorithm for Entry, Descent, and Landing Analysis

Sagliano, Marco und Theil, Stephan und D'Onofrio, Vincenzo und Bergsma, Michiel (2017) SPARTAN: A Novel Pseudospectral Algorithm for Entry, Descent, and Landing Analysis. In: 4th CEAS Eurognc Conference. 4th EuroGNC Conference, 25-27 Apr 2017, Warsaw, Poland.

[img] PDF - Requires a PDF viewer such as GSview, Xpdf or Adobe Acrobat Reader
751kB

Kurzfassung

In the last decades the theoretical development of more and more refined direct methods, together with a new generation of CPUs, led to a significant improvement of numerical approaches for solving optimal-control problems. One of the most promising class of methods is based on Pseudospectral Optimal Control. These methods not only provide an efficient algorithm to solve optimal-control problems, but also define a theoretical framework for linking the discrete numerical solution to the analytical one in virtue of the covector-mapping theorem. However, sveral aspects in their implementation can be refined. In this framework SPARTAN, the first European tool based on flipped Radau pseudospectral methods, has been developed. The tool, and the method behind it include two novel aspects. First, the discretized problem is automatically scaled with a novel technique, called Projected Rows Jacobian Normalization. This avoids ill-conditioned problems, which could lead to non-reliable solutions. Second, the structure of the Jacobian matrix is exploited, and the dual-number theory is used for its computation. This yields faster and more accurate solutions, since the associated Jacobian matrix computed in this way is exact. Two concrete examples show the validity of the proposed approach, and the quality of the results obtained with SPARTAN.

Dokumentart:Konferenzbeitrag (Vorlesung)
Titel:SPARTAN: A Novel Pseudospectral Algorithm for Entry, Descent, and Landing Analysis
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iD
Sagliano, Marcomarco.sagliano@dlr.dehttps://orcid.org/0000-0003-1026-0693
Theil, Stephanstephan.theil@dlr.dehttps://orcid.org/0000-0002-5346-8091
D'Onofrio, Vincenzovincenz.donofrio@gmail.comhttps://orcid.org/0000-0003-1026-0693
Bergsma, MichielNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:25 April 2017
Erschienen in:4th CEAS Eurognc Conference
Referierte Publikation:Ja
In Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:Optimal Control, pseudospectral methods, trajectory optimization
Veranstaltungstitel:4th EuroGNC Conference
Veranstaltungsort:Warsaw, Poland
Veranstaltungsart:internationale Konferenz
Veranstaltungsdatum:25-27 Apr 2017
Veranstalter :The Council of European Aerospace Societies
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Raumtransport
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R RP - Raumtransport
DLR - Teilgebiet (Projekt, Vorhaben):R - Flugexperiment Newfex
Standort: Bremen
Institute & Einrichtungen:Institut für Raumfahrtsysteme > Navigations- und Regelungssysteme
Hinterlegt von: Sagliano, Marco
Hinterlegt am:03 Mai 2017 11:34
Letzte Änderung:19 Okt 2017 10:43

Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags

Blättern
Suchen
Hilfe & Kontakt
Informationen
electronic library verwendet EPrints 3.3.12
Copyright © 2008-2017 Deutsches Zentrum für Luft- und Raumfahrt (DLR). Alle Rechte vorbehalten.