Reliable Fault Identification for Aircraft Control Surface Damage

Myala, J and Patel, Vijay V and Singh, GK (2019) Reliable Fault Identification for Aircraft Control Surface Damage. In: 6th Indian Control Conference, ICC 2019 - Proceedings, 18-20 December 2019, Hyderabad, India.

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Official URL: https://ieeexplore.ieee.org/document/9123243

Abstract

Fault Detection and Diagnosis system (FDD) is used to isolate the aircraft fault which provides information to reconfiguration mechanism to recover its operation during the fault occurrence. Using FDD, only anticipated faults can be tackled by design. Inaccurate information from the FDD and if interpreted incorrectly by the reconfiguration mechanism, can lead to a complete loss of system stability. Robust fault identification methods need to be explored especially for the unanticipated fault scenarios. In this paper, single control surface damage fault scenario arising due to either bird strike or battle damage is considered. A typical mathematical model of the aircraft is simulated with single control surface damage which captures the dynamics of high performance aircraft. The real-time parameter estimation of augmented aircraft is essential for reconfigurable flight control. Fault detection and identification is solved with extended Kalman filter considering only state and observation equations for lateral and directional axis.

Item Type: Conference or Workshop Item (Paper)
Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
AERONAUTICS > Aircraft Stability and Control
ENGINEERING > Electronics and Electrical Engineering
ENGINEERING > Mechanical Engineering
Depositing User: Mrs SK Pratibha
Date Deposited: 23 Nov 2021 11:43
Last Modified: 23 Nov 2021 11:43
URI: http://nal-ir.nal.res.in/id/eprint/13328

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