Rover Integrity

Rover Integrity

Shows integrity of selected rovers

Company:	<company name>
Operator:	N/A (scheduled report)
Address:	<company address>
	<city, postal code>
	<country, state>
Creation Date:	12/21/2022 12:30:11 AM
Time System:	GPS time
Report Interval:
Start Time:	12/20/2022 12:00:00 AM
End Time:	12/21/2022 12:00:00 AM
Duration:	1 Day(s), 0 Hour(s)

Statistics Configuration

Configuration name	Default
Use good only positions	Yes
Statistics dimensions	3D
Weighted statistics	Yes
Position threshold [m]	0.1000
Position quality filter	Fixed or converged
Quality determination	Position fixed
Consecutive positions for fix status	3

Rover Selection

Rover ID	Station Code	System	Description	X [m]	Y [m]	Z [m]
rtk engine [femern_vrs]_rri1	RRI1	ITRF2005		3625955.2744	728341.1925	5179034.7009

Position statistics
Offsets

Rover ID	# Good Positions	# Bad Positions	OffsetE [m]	OffsetN [m]	OffsetH [m]	Offset2D [m]	Offset3D [m]
rtk engine [femern_vrs]_rri1	85686	0	0.0006	-0.0018	-0.0067	0.0028	0.0077

RMS

Rover ID	# Good Positions	# Bad Positions	RMSE [m]	RMSN [m]	RMSH [m]	RMS2D [m]	RMS3D [m]
rtk engine [femern_vrs]_rri1	85686	0	0.0015	0.0027	0.0077	0.0031	0.0083

Standard deviation

Rover ID	# Good Positions	# Bad Positions	StDevE [m]	StDevN [m]	StDevH [m]	StDev2D [m]	StDev3D [m]
rtk engine [femern_vrs]_rri1	85686	0	0.0014	0.0020	0.0037	0.0014	0.0033

95% Values

Rover ID	# Good Positions	# Bad Positions	95%E [m]	95%N [m]	95%H [m]	95%2D [m]	95%3D [m]
rtk engine [femern_vrs]_rri1	85686	0	0.0031	0.0051	0.0133	0.0054	0.0137

Minima

Rover ID	# Good Positions	# Bad Positions	MinE [m]	MinN [m]	MinH [m]	Min2D [m]	Min3D [m]
rtk engine [femern_vrs]_rri1	85686	0	-0.0080	-0.0113	-0.0251	0.0000	0.0001

Maxima

Rover ID	# Good Positions	# Bad Positions	MaxE [m]	MaxN [m]	MaxH [m]	Max2D [m]	Max3D [m]
rtk engine [femern_vrs]_rri1	85686	0	0.0079	0.0086	0.0144	0.0119	0.0252

Init Time Statistics

Rover ID	# Good Init	# Bad Init	Reliability [%]	Mean [s]	68% [s]	95% [s]	99.7% [s]	Min [s]	Max [s]

Position Charts

Scatter Plot

Number of Satellites

PDOP