Abstract

Flight control system consists of flight controller, sensor, and actuator. Currently, the research focuses on the design and optimization of flight controller, regardless the influence of actuator. This paper is devoted to find out the way actuator effects the flight control system in both dynamic and energy consumption by substituting actuator (hydraulic actuator and electro-hydrostatic actuator) model into the model of flight control system. Results revealed that the model with electro-hydrostatic actuator is better than another in energy consumption characteristics, but worse in dynamic characteristics.

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 call

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.