Simulation research for flap skew on a certain type of aircraft
This paper describes the different kinds of flap skew malfunctions and principles of flap skew sensor monitoring on an aircraft. Taking a certain type of aircraft as an example, a flap system model is established by Simulink platform. Based on this model, the skew malfunctions can be simulated. The simulation results show that the established flap system model is effective, which lays a foundation for further research.
Authors
- Xianyu Wang (ORCID: https://orcid.org/0000-0002-5347-634X)
Institutions
- Commercial Aircraft Corporation of China (China) (CN)
Publication Details
- Journal
- IET conference proceedings.
- Published
- 2025-01-01
- DOI
- https://doi.org/10.1049/icp.2024.3153
- Citations
- 1
- Primary Topic
- Automotive and Human Injury Biomechanics
- Type
- article
- Field-Weighted Citation Impact
- 1.52