A problem about VTOL transition without a air speed sensor?
I have built a delta wing ,as following Fig.
I have set the parameters according to this two page 1)VTOL’S WITHOUT AIRSPEED SENSOR.2)TBS Caipiroshka.I have conducted indoor test and outdoor test.Now the plane can hover well .But MC-FW transition is failed !!
#The problem is:
when I Toggle transition RC switch which channel is assigned to AUX1,but the ailerons don’t response to the RC yaw and pitch input ,and then the plane is not under control.How to solve this problem？