Aircraft landing gear systems are essential to safe and efficient flight operations, as they operate under demanding conditions during takeoff, landing, and ground maneuvers. Because they are exposed to high loads and repeated stress, their reliability has a direct impact on safety, maintenance planning, and overall operational performance. This study explores the use of three decision-support approaches, namely the Analytic Network Process (ANP), the Decision-Making Trial and Evaluation Laboratory (DEMATEL), and an adapted Fuzzy Cognitive Map (FCM), to examine a critical landing gear subsystem. The analysis identifies the most influential engineering management factors affecting subsystem reliability and compares how the three methods capture factor importance and interdependencies. The results show that maintenance planning efficiency, failure mode criticality, cost of downtime, and workforce coordination consistently emerge as key reliability-related dimensions. The adapted FCM provides a broader uncertainty-aware representation of indirect causal propagation, while ANP supports prioritization through network-based weighting and DEMATEL highlights cause–effect structures among the factors. Overall, the findings demonstrate that combining these complementary methods can strengthen reliability-oriented decision-making by clarifying which factors should receive priority in maintenance, operational planning, and management strategies.
The implementation of the ground deceleration function in civil aircraft represents a critically complex process that deeply relies on the seamless collaboration of multiple onboard systems, including but not limited to braking, thrust reversal, spoiler, and steering systems. The operational logic governing these syste...
Mingqian Wang, Q. Yu, Miao Yu et al.· SAE technical paper series· 0 citations
This paper presents a validation framework for automated aircraft mass and balance operations, combining statistical process control with integrated risk scoring and addressing the critical gap between traditional centralised load control and emerging automated operations. A dual-validation system integrates univariate...
Ivan Jakovljević, O. Čokorilo, Ljubiša Vasov· Engineer· 0 citations
The dynamic reconfigurability of civil aircraft flight control systems (FCS) enhances mission adaptability yet introduces significant operational uncertainty. Traditional static safety assurance methods often fail to cope with such real-time variations. To address this, this paper proposes an integrated safety assuranc...
Wenshen Peng, Jun-Ran Wang, Kai Xue et al.· Proceedings of the Instituti...· 0 citations
Aircraft landing gear systems are characterized by strong nonlinearity, multi-physics coupling, and significant uncertainty. This paper reviews representative modeling approaches, including multibody dynamics, rigid–flexible coupling modeling, multi-domain unified modeling, co-simulation, and tire–runway coupled modeli...
Zhu Cheng· Applied and Computational En...· 0 citations
The modern multi-domain battlespace increasingly demands cost-effective, persistent platforms for Forward Air Control (Airborne) (FAC(A)) and Close Air Support (CAS) missions. While utilizing Commercial Derivative Aircraft (CDA) presents a viable alternative to high-maintenance military assets, the specific aerodynamic...
Süleyman Murat Köroğlu, İlker Ünlü, I. Özkol· Aerospace· 0 citations
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