FM847

Looking at the Restart states from Rev 848 we have the following results for FM847.
FM847		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	SMA error	Plane change error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)			
MMS1	Feb 08 2018 07:19:08.581	84221.407	84221.407	84221.426	0.000	0.019	-0.01854			
MMS2	Feb 08 2018 07:18:57.318	84221.338	84222.267	84222.326	0.930	0.988	-0.05881	-6.327%	4.791%	
MMS3	Feb 08 2018 07:18:59.106	84221.330	84221.008	84221.028	-0.322	-0.302	-0.01973	6.126%	1.880%	
MMS4	Feb 08 2018 07:19:04.532	84221.380	84216.320	84216.325	-5.059	-5.054	-0.00483	0.095%	-8.915%	
 
MMS2 was 0.054 m/s (net delta-v) and 37.20% axial, MMS3 was 0.11 m/s and 55.51% axial, and MMS4 was 0.11 m/s and 29.53% axial.
Small plane change (especially MMS4) and small SMA changes (MMS2 and MMS3) lead to large % errors.  

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.
As shown in the table below, all maneuvering spacecraft meet the requirement except MMS3 DVX and DVY, MMS2 DVY
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)	
MMS4_FM847	2018_37/12:01:12 to 2018_37/12:01:22	0.0986	-0.0526	0.0196	
		0.01	0.01	0.01	
		-0.001357	-0.003554	0.0003862	
MMS3_FM847	2018_37/15:11:12 to 2018_37/15:11:32	-0.0275	-0.0083	-0.1054	
		0.01	0.01	0.01	
		0.01468	0.0173	0.0005361	
MMS2_FM847	2018_37/16:46:12 to 2018_37/16:46:12	-0.0364	-0.0069	-0.0383	
		0.01	0.01	0.01	
		0.009789	-0.01315	0.0004999