2015 summer semester team F 8thJuly 06, 2015


I will talk about the 3rd test flight on July 6. In the 2nd test flight, we adjusted gain parameters related gyro control. In the 3rd test flight, we adjusted gain parameters related accelerometer control. If accelerometer control doesn’t work, the airframe tilts and the position becomes unstable. We adjusted gain parameters and conducted test flights many times, but didn’t realize desirable movement. As a reason for this, we suspect a voltage drop of the battery and an individual difference between the motors and plan to debug them.

Department of Mechanical Engineering.
Hiroyuki Karasawa