Dynamic Lever Arm Error Compensation of POS Used for Airborne Earth Observation

Table 2

Calibration result of the experiment system in Figure 5.

		x	y	z
First-level rigid lever arm (m)		−1.738	−3.503	2.537
Second-level dynamic lever arm (m)	Rigid lever arm	−0.008	0.553	−0.136
	Rotation lever arm	0.0633	0.001	0.001
Initial transformation matrix
Initial transformation matrix
Initial output angle (°)		42.812