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

Table 1

Calibration result of the experiment system in Figure 4.

		x	y	z
First-level dynamic lever arm (m)	Rigid lever arm	3.547	−3.090	2.030
	Rotation lever arm	−0.117	0.512	0.042
Second-level rigid lever arm (m)		−0.288	0.526	0.180
Initial transformation matrix
Initial output angle (°)		57.105