Self-Compensation for Disturbances in Differential Vibratory Gyroscope for Space Navigation

Table 1

Shock test summary table.

Rejection factor in terms of peak value		Rejection factor in terms of angle error, max error (arcmin)	Rejection factor in terms of bias change, max bias change (deg/s)		Diff. CVG bias sensitivity to shock accel. (deg/s/)
Shock amplitude 20 , 2 ms duration
Along IA	Lateral	Along IA	Along IA	Lateral	Lateral
2	2	5	3	8	10^-3
		2	0.06	0.03