Abstract
Aircraft's ground manoeuvrability is directly influenced by its steering control system. Nose landing gear steering system is used for major aircrafts, while main landing gear collaborative steering system is commonly introduced to wide-body aircrafts, proposed to decrease the main landing gear steering torque, decrease the turning radius, and improve the tire wearing performance. In this paper, the hydraulic system proposal and control strategy is raised for a downscaling test-rig, which is designed to estimate the main landing gear steering control system. Finally, a AMESim simulation model is built evaluate the collaborative performance.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
