Center for Mapping



Kinematic Test

 

In order to test the GPS hardware in the production environment, kinematic data, collected on July 13, 2000 on the stretch of the state highway 315 were processed, and the results are presented here for the comparison with the static case.  During this test only Trimble 4000SSI and 4000SSE and Topcon Legacy were used, all connected to a single compact L1/L2 Trimble antenna with ground plane, using a 4-way splitter.

 

Table 1 presents the survey statistics in terms of number of kinematic segments processed, gaps duration, total number of fixes along the trajectories, and type of solution selected automatically by the GPSurvey processing engine, based on data quality and distance to the base station (ionosphere free combination is used for base-rover separation of 5 km and more). Figures 1 and 2 illustrate the satellite observability and continuous kinematic RMS for 4000SSI and Topcon/JPS Legacy receivers during the common/overlapping time window. Both receivers were in motion at that time, recovering from the loss of lock caused most probably by severe multipath and interference. The Trimble receiver picked up the signal at 16:53 after a 7-minute gap, and continued tracking the satellites until 17:36, while Legacy picked up a signal at 16:51:59 (after about 5-second gap) and continued tracking until 17:41.

 

Receiver type

Solution segments

Gaps between segments

[min]

Total number of points

 

Solution type

 

Trimble 4000SSE

16:10 – 16:41

16:41 – 16:46

16:53 – 17:36

17:44 – 18:04

 

0

7

8

1812

322

2493

1195

Iono free fixed DD

Iono free fixed DD

Iono free fixed DD

Iono free float DD

Total

99 min

15

5822

 

 

Trimble 4000SSI

16:10 – 16:37

16:37 – 16:41

16:41 – 16:46

16:53 – 17:36

17:44 – 18:04

 

0

0

7

8

1600

217

316

2533

1186

Iono free fixed DD

Iono free float DD

Iono free fixed DD

Iono free fixed DD

Iono free float DD

Total

99 min

15

5952

 

 

Topcon/JPS Legacy

16:10 – 16:41

16:41 – 16:46

16:47 – 16:52

16:52 – 17:41

17:44 – 18:04

 

0

1

0

3

1806

327

217

2834

1150

Iono free float DD

Iono free float DD

Iono free float DD

Iono free float DD

Iono free float DD

Total

110 min

4

6334

 

 

Table 1. Statistics of the kinematic test of July 13, 2000: antenna splitter and a single Trimble L1/L2 antenna with ground plane were used.

 

 

 

 

 

 

 

 


Figure 1. Satellite visibility for 4000SSI (left) and Legacy (right) during the time window 16:53 – 17:36 (4000SSI) and 16:52 – 17:41 (Legacy).

 

 

 

 

 

 

 

 


Figure 2. Continuous kinematic RMS for 4000SSI (left) and Legacy (right) during the time window 16:53 – 17:36 (4000SSI) and 16:52 – 17:41 (Legacy).

 

Even though Legacy seems to be able to restart and continue tracking somehow better as compared to 4000SSI/SEE, the level of measurement residuals provided by Legacy is higher, as can be observed in Figure 2. Also, due to the higher noise level, only a float solution is available from the Legacy data (Table 1). Moreover, residual plots based on Legacy data experience sometime distinct peaks, which might indicate data outliers. It should also be mentioned that the solution provided by Legacy during the time window of 16:47 – 16:52, when other receivers lost lock, displays position RMS reaching 22 – centimeter level, and some parts of the solution are obviously based on the Kalman filter prediction only, as observability chart shows some gaps in the signal, illustrated in Figure 3.

 


                                   

                                            Figure 3. Satellite visibility for Legacy during the time window 16:47 – 16:52.

 

Problem Overview| Receiver Performance Considerations| Static Tests| Kinematic Tests