Macm_020171
Aerospace
Hello community,
I wanted to know how electric actuators in light aircraft stops the rotation of the control surface to the motion limit +/- deg. Are actuators including an integrated stop system (electronic or mechanical)? Or this stopping feature has to be integrated into the airframe?
Thank you!
I wanted to know how electric actuators in light aircraft stops the rotation of the control surface to the motion limit +/- deg. Are actuators including an integrated stop system (electronic or mechanical)? Or this stopping feature has to be integrated into the airframe?
Thank you!