The controller design for permanent magnet motor with complete electrical double redundancy structure

Yong, Zhou; Chen, Long; Wang, Jiayao; Zhang, Chao

doi:10.1109/phm.2017.8079138

Cited by 3 publications

(1 citation statement)

References 6 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…The digital servo controller also undertakes servo control and margin management. The controller can control the servo motion of the servo by integrating the output signal of the position sensor (Zhou et al 2017).…”

Section: Flight Control System Actmentioning

confidence: 99%

Extending Model-Based Systems Engineering into Integrated Platform Designed for Civil Aircraft Develop

Wang

Zhang

et al. 2021

J. Aerosp. Technol. Manag.

View full text Add to dashboard Cite

With the continuous development and application of modeling technology, civil aircraft designers urgently need to apply model-based systems engineering (MBSE) theory and methods into the field of civil aircraft development. However, the existing modeling tools, which combined with MBSE methodologies, only focus on one particular area, such as requirement modeling, functional modeling and design synthesis. This kind of low coupling design system makes it difficult to link the upstream and downstream designers in the early stage of system development. This paper introduces the MBSE development process of civil aircraft and then establishes an integrated platform composed of six work stations for civil aircraft development based on this process. Commercially available modeling tools, such as IBM Rational DOORS and enterprise architect (EA), are conducted in the platform. The development of flight control system is taken as an example to test the feasibility and efficiency of our integrated platform in logic layer. This platform can complete the activities of aircraft life cycle function analysis, requirement and model management. The loose coupling between the modules and the high cohesive nature allows different system engineers to maintain their design independence and consistency at different stages of development.

show abstract

Section: Flight Control System Actmentioning

confidence: 99%