FR188

Looking at the Restart states from Rev 189 we have the following results for FR188.

FR188		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (m)		
MMS1	Sep 17 2015 15:06:24.760	42110.604	42110.604	42110.605	0.000	0.00126	-0.00124		
MMS2	Sep 17 2015 15:05:54.860	42110.593	42094.008	42093.999	-16.586	-16.59460	0.00875	-0.05%	
MMS3	Sep 17 2015 15:08:20.017	42110.585	42138.134	42138.096	27.549	27.51178	0.03740	0.14%	
MMS4	Sep 17 2015 15:05:52.571	42110.593	42073.452	42073.409	-37.141	-37.18396	0.04294	-0.12%	

The Table below provides the following information:
•	First row for each maneuver: planned maneuver total delta-V values based on the associated DVTABLEs  
•	Second row for each maneuver: associated final maneuver planning requirements 
•	Third row for each maneuver: predicted velocity error at the time of the maneuver computed by differencing the predicted velocity at the maneuver time (starting with the post-perigee GEONS state prior to the maneuver) vs the definitive GEONS state at the time of the maneuver.
The predicted velocity meets all requirements with significant margin.
Maneuver ID	Timespan	DVX (m/s)/ 
Req. (m/s)/
DiffVX(m/s)	DVY (m/s)/
Req. (m/s)/
DiffVY(m/s)	DVZ (m/s)/
Req. (m/s)/
DiffVZ(m/s)	
MMS2_FR188	259/07:10:35– 259/07:21:45	-1.787229	-0.378769	3.843861	
		0.017	0.010	0.038	
		0.002	0.002	0.001	
MMS4_FR188	259/08:40:35- 259/08:46:25	-3.544442	1.812002	2.227121	
		0.035	0.018	0.022	
		<0.001	<0.001	<0.001	
MMS3_FR188	259/18:15:35- 259/18:21:35	1.820845	3.371494	-0.617583	
		0.018	0.033	0.010	
		<0.002	<0.002	<0.001	

All FR188 and FR189 maneuvers were planned using predicted ephemeris files based on GEONS post-perigee RST vectors @ 2015-257/05:21.  Note that these predictions start 2+ orbits prior to FR188 and 3+ orbits prior to FR189 because the FR188 maneuvers started only a couple of hours post-perigee,  CAM was held the prior day, and final maneuver plans had to be prepared prior to the CAM.