TY - GEN
T1 - Analysis of Controller Errors in an Asynchronous, Redundant Flight Control System
AU - Hofsäß, Hannes
AU - Holzapfel, Florian
N1 - Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2022
Y1 - 2022
N2 - Redundancy is a common means in the design of flight control system architectures, to meet demanding safety objectives for safety-critical applications. Redundancy management provides fault tolerant system operation when introducing redundancy to the system. In an asynchronous system, inherent signal errors introduced to the system due to timing offsets can affect the excitation of signals used for failure monitoring and redundancy management. In this work, we present the frequency domain analysis of the inherent errors in redundant controller outputs that result from timing offsets in an asynchronously operating flight control system. For an abstracted redundant system, we derive the transfer functions for the controller output error excited by pilot inputs and analyze the effects of different operational sequences also considering state equalization. We present several observations and perform the analysis for the closed-loop dynamics of a large drone model. The observations are validated in time domain with numerical simulations.
AB - Redundancy is a common means in the design of flight control system architectures, to meet demanding safety objectives for safety-critical applications. Redundancy management provides fault tolerant system operation when introducing redundancy to the system. In an asynchronous system, inherent signal errors introduced to the system due to timing offsets can affect the excitation of signals used for failure monitoring and redundancy management. In this work, we present the frequency domain analysis of the inherent errors in redundant controller outputs that result from timing offsets in an asynchronously operating flight control system. For an abstracted redundant system, we derive the transfer functions for the controller output error excited by pilot inputs and analyze the effects of different operational sequences also considering state equalization. We present several observations and perform the analysis for the closed-loop dynamics of a large drone model. The observations are validated in time domain with numerical simulations.
UR - https://www.scopus.com/pages/publications/85135063894
U2 - 10.2514/6.2022-3232
DO - 10.2514/6.2022-3232
M3 - Conference contribution
AN - SCOPUS:85135063894
SN - 9781624106354
T3 - AIAA AVIATION 2022 Forum
BT - AIAA AVIATION 2022 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA AVIATION 2022 Forum
Y2 - 27 June 2022 through 1 July 2022
ER -