Since the last decade, aircraft systems, such as flight control and landing gear, have been
requiring increasing power, and consequently, the complexity of hydraulic aircraft systems …

The Kalman filter plays an important role in the field of aero‐engine control system fault
diagnosis. However, the design of the Kalman filter bank is complex, the structure is fixed …

IN RECENT years, several technologies have been developed to improve postfailure flight
safety [1–3]. Most of the research toward this end includes high-performance real-time fault …

This paper proposes a framework for aircraft fault diagnosis based on the offline analysis of
flight data. It overcomes the limitations of current data-driven approaches by combining …

This paper presents a Matlab/Simulink simulation environment developed at West Virginia
University to facilitate the design, testing, and analysis of fault-tolerant control laws for …

This paper presents the development of a biologically inspired generalized conceptual
framework for the detection, identification, evaluation, and accommodation of aircraft …

Failures, malfunctions, and damage affecting aircraft subsystems, as well as general
environmental and dynamic upset conditions, have been consistently identified as the …

Multiple air-data sensors placed on different positions on an aircraft are usually expected to
provide identical measurements. This is because aircraft are assumed to fly in no-wind or …

This paper develops a new active fault‐tolerant control system based on the concept of
analytical redundancy. The novel design presented here consists of an observation filter …

In this paper, two approaches are proposed and compared for the detection and
identification of aircraft subsystem failures based on the artificial immune system paradigm …