Abstract

PHM technology plays an increasingly significant role in modern aviation condition-based maintenance. As an important part of prognostics and health management (PHM), a health assessment can effectively estimate the health status of a system and provide support for maintenance decision making. However, in actual conditions, various uncertain factors will amplify assessment errors and cause large fluctuations in assessment results. In this paper, uncertain factors are incorporated into flight control system health assessment modeling. First, four uncertain factors of health assessment characteristic parameters are quantified and described by the extended λ-PDF method to acquire their probability distribution function. Secondly, a Monte Carlo simulation (MCS) is used to simulate a flight control system health assessment process with uncertain factors. Thirdly, the probability distribution of the output health index is solved by the maximum entropy principle. Finally, the proposed model was verified with actual flight data. The comparison between assessment results with and without uncertain factors shows that a health assessment conducted under uncertain conditions can reduce the impact of the uncertainty of outliers on the assessment results and make the assessment results more stable; therefore, the false alarm rate can be reduced.

Highlights

  • Accepted: 25 October 2021The maintenance mode of modern aircraft is changing from scheduled to conditionbased maintenance (CBM)

  • (3) Uncertainty propagation based on Monte Carlo simulation (MCS): According to the PDF of each characteristic generate random numbers with theof same distribution as the input ofaccordin the

  • prognostics and health management (PHM) technology has become an important tool to ensure the operation of modern commercial aircraft, because it can provide a large amount of fault information for maintenance decision making, and as an important part of PHM technology health assessments can accurately assess the operational status of aircraft

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Summary

Introduction

The maintenance mode of modern aircraft is changing from scheduled to conditionbased maintenance (CBM). Mirko Mazzoleni [9] presents a health-monitoring approach for electromechanical actuators (EMAs) and verifies the approach using a dataset collected from a large experimental campaign on a 1:1 scale EMA for primary flight controls of small aircrafts These studies have mostly conducted health assessments under certain conditions, such as complete failure characteristics, known degradation data distribution, etc. The objective of this paper is to establish a health assessment model of a flight control system under uncertain conditions and obtain the probability distribution of its health index. By comparing the results of the health assessment under certain and uncertain conditions, the validity of the proposed method is obtained. The final section analyzes the results and presents the conclusion of the whole paper

Basic Theory
Establishing Health Assessment Indicators
Dividing Health
Assessment Model—Fuzzy Comprehensive Assessment Model
Objective Weighting Method Based on Rough Set Reduction
Flight Control System Health Assessment Process
Flight Control System Health Assessment under Uncertainty
Uncertainty Quantification
Uncertainty Propagation Based on MCS
Probability Distribution Based on the Maximum Entropy
Flight Control System Health Assessment Process under Uncertain Conditions
Results and Discussion
Flight Control System Assessment of a Single Flight
Discussion
Conclusions
Full Text
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