Aug 2026· Engineer· Vol 7, pp. 379· 0 citations· 25 references
Abstract
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 control limits, a weighted multivariate T2-type statistic, and composite scoring with operational risk assessment; risk scoring quantifies centre of gravity proximity and maximum mass margins. The framework was validated using 48 flights operated by Airbus A350-900/1000 aircraft. The framework was evaluated using a two-phase design—flights 1–30 for calibration (Phase I) and flights 31–48 for prospective evaluation (Phase II). Across all 48 flights it yields an 81.25% automation-eligibility rate (39 GREEN), with 4.17% YELLOW (non-blocking supervisor notification within a defined service window) and 14.58% RED (mandatory review). RED cases result from cargo offloads, dangerous goods changes, or significant baggage/ZFW variations, while cargo operations show exceptional stability (the exclusively cargo-loaded Compartment 2 has σ = 9 kg, versus 219 kg for total cargo). The framework enables transition from centralised load controller roles to exception-based supervision, with risk scoring outputs driving targeted, proportional safety measures. To the best of the authors’ knowledge, it provides the first systematic method for determining when automated load control can be trusted without human intervention—a critical requirement as the industry transitions towards full automation.
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 op...
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Specific aircraft services, such as transport, exist in a wide range of safety targets. This paper analyses a safety assessment method applicable to both manned and unmanned aircraft, offering the following contributions. First, different aircraft types, services, and current specifications have been reviewed and con...
Mingyang Huang, Ming-Kan Zhang, Lintong Li et al.· Proceedings of the Instituti...· 0 citations
Uncrewed aerial vehicles (UAVs) represent a promising alternative for building facade cleaning, improving efficiency while reducing the risks associated with working at height. However, such operations are particularly challenging due to the reaction forces generated by fluid discharge, which can compromise UAV stabili...
Gálata Martínez-Alonso, E. Aldao, F. Veiga-López et al.· Drones· 0 citations
This paper investigates the flight test method for the high speed characteristic – dive to VDF/MDF on civil transport category aircraft equipped with high-speed protection functions. The existing CCAR 25.335(b)(1) does not address the influence of high-speed protection, which may prevent the aircraft from maintaining t...
Hou-Shi Wang, Yuan-Tao Fu· Journal of Physics, Conferen...· 0 citations
The research results indicate that integrating digital twin architecture with model-driven design can effectively mitigate insufficient accuracy in single-domain modeling, and can provide clear ideas and references for optimizing multi-domain coupled modeling of aircraft and the digital development of flight control eq...
Yuxuan Zhu· Applied and Computational En...· 0 citations
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