I'm trying to come up with a safe procedure to accurately determine stall airspeed for a plane with an airspeed sensor and ardupilot logging. Any feedback on this technique?
1. Achieve stable level flight in full manual
2. Reduce throttle
3. Increase angle of attack to maintain altitude
4. Goto Step 2. until no longer able to maintain altitude
5. Stall has occurred, increase throttle and reduce angle of attack
6. Review flight logs to determine airspeed when control authority was lost
Replies
you also might want to see how well the air speed sensor works at angles of attack near stall.... the static port should be fine but the pitot port might see larger pressure changes. depending on your plane, you can also take a pretty good wag at calculating stall speed based on wing loading and your wing's max Cl.
how accurately do you want to know it?
this is also a handy reference for understanding stall performance: http://www.aviation.org.uk/docs/flighttest.navair.navy.milunrestric...