I. Introduction
During long-term airplane operation, the landing gear system, frequently subjected to complex and variable mechanical stresses, accumulates fatigue damage, impacting takeoff, landing safety, and flight performance. Load monitoring is pivotal in ensuring flight safety and reliability, offering real-time stress state feedback to enable preventive maintenance, mitigating structural failure and accelerated fatigue due to overload [1], [2], [3], [4], [5], [6]. In addition, load monitoring data validate design-stage load estimation accuracy, assessing in-service load capacity against design expectations [7], [8], thereby preventing safety hazards stemming from underestimated design loads. Advancing beyond traditional strain-based regression coefficient calculations and sensor installations [9], [10], [11], modern load monitoring technology evolves toward increased intelligence and efficiency.