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Control System Design of the Lander Demonstrator EAGLE

Leite Filho, W. C. and Dumke, Michael and Theil, Stephan (2015) Control System Design of the Lander Demonstrator EAGLE. EUCASS 2015, 29 June - 3 July, 2015, Krakow, Poland.

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This paper presents the control system design for a prototype demonstrator of a small moon lander. The deflection of the main thruster is used to obtain the lateral displacement control while the actual value of the thrust is controlled to get hovering. To guarantee the decoupling of maneuver planes and increase the stability margin, a roll control system is included which uses a cold gas system as auxiliary thruster (on-off actuators). The algorithms are discussed and the computation of gains is presented. Simulation results also are shown.

Item URL in elib:https://elib.dlr.de/98442/
Document Type:Conference or Workshop Item (Speech)
Title:Control System Design of the Lander Demonstrator EAGLE
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Leite Filho, W. C.Instituto de Aeronáutica e Espaço IAEUNSPECIFIED
Dumke, MichaelDLR-RY, BremenUNSPECIFIED
Theil, StephanDLR-RY, BremenUNSPECIFIED
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:EAGLE Control System Simulation
Event Title:EUCASS 2015
Event Location:Krakow, Poland
Event Type:international Conference
Event Dates:29 June - 3 July, 2015
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space System Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Space System Technology
DLR - Research theme (Project):R - Lageregelungstechnik / Formationsflug (old)
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Navigation and Control Systems
Deposited By: Dumke, Michael
Deposited On:06 Oct 2015 10:43
Last Modified:10 May 2016 23:32

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