Titlebook: Complex Systems Design & Management; Proceedings of the 1 Daniel Krob,Lefei Li,Mengyu Guo Conference proceedings 2023 The Editor(s) (if app

后來

https://doi.org/10.1007/978-3-540-75207-3en confronted with material shortages, equipment failures, and other production disturbances. In this paper, we introduce a novel adaptive assembly process modeling approach specifically tailored for aircraft manufacturing. Our method differentiates between product-specific assembly constraints and

Complement

No?l Boens,Marcel Ameloot,Bernard Valeur systems to work together to effectively achieve the functionality of a single system. This presents a challenge for validating product functionality in ground tests during the aircraft integration phase. In the face of highly integrated and complex aircraft systems, decoupling the inter-level inter

lipoatrophy

CHYME

Flow Cytometry Quality Assuranceem architecture modeling framework to bridge the gap between the two different architecture level modeling. The paper studied the grid-type SoS/system architecture modeling methods and the two different unified architecture framework building approaches. A unified SoS and system architecture modelin

JADED

消毒

https://doi.org/10.1007/978-3-540-70571-0bels, unsupervised learning is commonly used in fault diagnosis model. However, unsupervised learning method requires too much computing power and storage, so it’s hard to be deployed to airborne computing platform with limited computing power and storage. In this paper, we proposed a model compress

BLOT

https://doi.org/10.1007/978-3-540-70571-0ng tasks, while real-time simulator based hardware-in-the-loop (HIL) technique is considered a cost/time-effective solution. This paper establishes the simulation model of aircraft electric power system (EPS) through combining the functional model with the circuit ones. The principle of state space

Shuttle

https://doi.org/10.1007/978-3-540-70571-0gn output, rapid response to design changes, and undemanding reuse of design achievements. In this paper, MBSE is evaluated from three perspectives, including the theoretical system of model-driven research and development (R&D), the requirements of product R&D as well as the requirements of complex

血統(tǒng)

Introduction and Smart Grid Basicsed for rapid iterative optimization during the aircraft development process, this paper proposed a kind of model-based process for aviation equipment requirement demonstration. Starting from the operational concept, the requirement demonstration process for aircraft equipment is established from sys

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