For the purpose of warehouse stock checking drone development, the automatic altitude control was reconsidered in comparison to human pilot control. The value of gains of PID feedback control were set separately in case that the quadrotor is above or under the command altitude, and is climbing up or descending down. The typical results are shown and discussed in this paper. The proposed technique could control the altitude within ± 0.3 m of error as well as normal human pilot.
Automatic Altitude Control of Multirotor Aircraft with Consideration of Motion
01.01.2019
140650 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch