elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Hardware-In-The-Loop Tests of Complex Control Software for Rocket Propulsion Systems

Waxenegger-Wilfing, Günther and Dresia, Kai and Oschwald, Michael and Schilling, Klaus (2020) Hardware-In-The-Loop Tests of Complex Control Software for Rocket Propulsion Systems. In: 71th International Astronautical Congress, IAC 2020. 71st International Astronautical Congress (IAC), 12.-14. Okt. 2020, Virtuell.

Full text not available from this repository.

Abstract

Software of rocket propulsion systems has a very high complexity but must also guarantee an outstanding level of reliability. Therefore, extensive tests are inevitable during the development process to meet the requirements. However, ground tests of the entire propulsion system are extremely expensive and can not address all nominal and off-nominal behavior that could possibly occur during the mission. Hardware-in-the-loop simulations allow realistic testing of embedded systems (e.g., the engine controller or an actuator) by combining a software simulation with emulated electrical sensor and actuator signals. This contribution discusses hardware-in-the-loop methods for anomaly detection and control systems of rocket propulsion systems. We develop a roadmap surveying a step-by-step approach to demonstrate the reliability of advanced control algorithms and sketch how to deploy such algorithms on space-graded embedded systems. In the future, adaptive and reconfigurable control for the propulsion system will become increasingly important. Adaptive control can tune the control actions to uncertain or changing system characteristics. Also, coupling the control algorithms to suitable anomaly detection systems allows the safe reaction to unforeseen events, which further improves the reliability of the propulsion system. The DLR Institute of Space Propulsion operates extensive test facilities for developing propulsion system technologies to operational maturity and ensuring their quality. Specific attitude pointing aspects of the propulsion system software can be simulated by high precision turntables at the company Zentrum für Telematik (ZfT). Within the cooperation between the DLR Institute and ZfT, different aspects of complex control software for propulsion systems are analyzed and tested using the available facilities.

Item URL in elib:https://elib.dlr.de/136877/
Document Type:Conference or Workshop Item (Speech)
Title:Hardware-In-The-Loop Tests of Complex Control Software for Rocket Propulsion Systems
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Waxenegger-Wilfing, Güntherguenther.waxenegger (at) dlr.dehttps://orcid.org/0000-0001-5381-6431
Dresia, KaiKai.Dresia (at) dlr.dehttps://orcid.org/0000-0003-3229-5184
Oschwald, MichaelMichael.Oschwald (at) dlr.dehttps://orcid.org/0000-0002-9579-9825
Schilling, Klausschi (at) informatik.uni-wuerzburg.deUNSPECIFIED
Date:October 2020
Journal or Publication Title:71th International Astronautical Congress, IAC 2020
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Rocket Engine Control, Control System Development, Rocket Propulsion Test Facilities, Hardware-In-The-Loop Simulation
Event Title:71st International Astronautical Congress (IAC)
Event Location:Virtuell
Event Type:international Conference
Event Dates:12.-14. Okt. 2020
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Wiederverwendbare Raumfahrtsysteme und Antriebstechnologie
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: Waxenegger-Wilfing, Günther
Deposited On:26 Oct 2020 06:36
Last Modified:26 Oct 2020 06:36

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.