Abstract
The use of flight tables and the present state of the art are described and the specifications for the flight table are derived. Major stress is laid on building a relatively cheap model, that will, nevertheless, satisfy the present requirements. A detailed description of the various alternatives that exist when deciding upon the major components is given along with a discussion on the linear design of the servo loops and stability validations for the expected nonlinearities. A grapho-analytical jump prediction is presented and the wiper backlash problem is analyzed.
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 callMore From: IEEE Transactions on Industrial Electronics and Control Instrumentation
Disclaimer: 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.
