TY - GEN
T1 - Enhancing the auto flight system of the SAGITTA Demonstrator UAV by fault detection and diagnosis
AU - Kugler, Martin E.
AU - Holzapfel, Florian
N1 - Publisher Copyright:
© 2015 IEEE.
PY - 2016/3/9
Y1 - 2016/3/9
N2 - The SAGITTA Demonstrator is a novel UAV with a digital flight control system being developed by the Institute of Flight System Dynamics of Technische Universitat Munchen. This paper presents the enhancement of the integrated auto flight system software by a monitoring / fault detection and diagnosis module. Its algorithms are designed to assess the health status of the flight control system components and to detect faults or failures. Within the scope of the simplex system architecture of the SAGITTA Demonstrator, monitoring / fault detection and diagnosis focuses on availability and accuracy of sensor values, detection of data link and flight control system-internal communication errors, and operability of the actuator control electronics. The developed module interconnects with the system automation and automatic take-off and landing modules of the auto flight system, which feature fault evaluation and predefined contingency procedures on the basis of the fault detection and diagnosis introduced in this paper.
AB - The SAGITTA Demonstrator is a novel UAV with a digital flight control system being developed by the Institute of Flight System Dynamics of Technische Universitat Munchen. This paper presents the enhancement of the integrated auto flight system software by a monitoring / fault detection and diagnosis module. Its algorithms are designed to assess the health status of the flight control system components and to detect faults or failures. Within the scope of the simplex system architecture of the SAGITTA Demonstrator, monitoring / fault detection and diagnosis focuses on availability and accuracy of sensor values, detection of data link and flight control system-internal communication errors, and operability of the actuator control electronics. The developed module interconnects with the system automation and automatic take-off and landing modules of the auto flight system, which feature fault evaluation and predefined contingency procedures on the basis of the fault detection and diagnosis introduced in this paper.
KW - ATOL
KW - Fault Detection and Diagnosis
KW - Flight Control System
KW - Monitoring
KW - Remotely Piloted Aircraft
KW - SAGITTA Demonstrator
KW - Simplex
KW - System Architecture
KW - System Automation
KW - UAV
UR - http://www.scopus.com/inward/record.url?scp=84966487039&partnerID=8YFLogxK
U2 - 10.1109/ICARES.2015.7429827
DO - 10.1109/ICARES.2015.7429827
M3 - Conference contribution
AN - SCOPUS:84966487039
T3 - Proceedings of the 2015 IEEE International Conference on Aerospace Electronics and Remote Sensing, ICARES 2015
BT - Proceedings of the 2015 IEEE International Conference on Aerospace Electronics and Remote Sensing, ICARES 2015
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - IEEE International Conference on Aerospace Electronics and Remote Sensing Technology, ICARES 2015
Y2 - 3 December 2015 through 5 December 2015
ER -