Control System Design for a Ducted-Fan Unmanned Aerial Vehicle Using Linear Quadratic Tracker

Table 2

Comparison of trim analysis results between wind tunnel test and mathematical modeling [13].

	()	RPM	(deg.)	(deg.)
Wind tunnel test	5	5880
	10	5844
	15	5752
Mathematical modeling	5	5907
	10	5647
	15	5602