Stability Precision Error Correction of Photoelectric Detection by Unmanned Aerial Vehicle

Table 2

Necessary parameters of the product for the experiment.

PARM	Descriptions	Values	Units
	Rotary inertia of the azimuth motor	0.02
	Rotary inertia of the azimuth load	0.04
	Rotary inertia of the pitch motor	0.01
	Rotary inertia of the pitch load	0.02
	Total resistor of the two armature circuits	8.60
	Total inductance of the armature circuits	0.01
	Damping coefficient of the two motors	10	/
	Elastic coefficient of the two motors	100000	/
	EMF coefficient of the two motors	0.33	/
	Motor torque coefficient of the two motors	0.33	/
	Amplification coefficient of driving circuit	20	/
	Resistor of the driving circuit	0.4
	Amplification coefficient of the gyroscopes	15/	/
	Natural frequency of the gyroscopes	200
	Damping coefficient of the gyroscopes	0.7	/