Abstract
This paper designs the quadrotor aircraft, and the software algorithm is the core. The software structure mainly uses the quaternion to Euler angle algorithm as the core to carry out the real-time attitude calculation of the aircraft, and supplemented by the cascade PID controller algorithm to stabilize, accurately and quickly respond to the RF signal. In this paper, the final goal of stable flight is achieved by solving the flight attitude algorithm.
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: IOP Conference Series: Materials Science and Engineering
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.
