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The flapping-wing aerial vehicle(FWAV) has appealed to more and more researchers recently owing to its outstanding performance in various domains and the development of some related technologies. The research on autonomous flight control of the FWAV involves many challenges and is still in nascent stages. In this work, we develop an FWAV with a mass of 14.1 g and build a vision-based experimental platform. A modelbased controller is proposed on the basis of theory and simulation results prove its effectiveness. A PID control algorithm based on visual measurement is utilized to achieve the height-keeping control of the FWAV, and a software platform is designed to record the flight status determined using Euler angles and position information.
The flapping-wing aerial vehicle (FWAV) has appealed to more and more researchers recently owing to its outstanding performance in various domains and the development of some related technologies. The research on autonomous flight control of the FWAV involves many challenges and is still in nascent A. This model is based on theory and simulation results prove its effectiveness. A PID control algorithm based on visual measurement is utilized to achieve the height-keeping control of the FWAV, and a software platform is designed to record the flight status determined using Euler angles and position information.