FM912

Looking at the Restart states from Rev 913 we have the following results for FM912
FM912		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	Aug 10 2018 09:08:29.244	84264.688	84264.688	84264.716	0.000	0.028	-0.02803			
MMS2	Aug 10 2018 09:08:06.191	84264.632	84256.874	84256.960	-7.758	-7.672	-0.08603	1.109%	0.399%	
MMS3	Aug 10 2018 09:08:51.000	84264.680	84262.993	84263.023	-1.687	-1.657	-0.02949	1.748%	-0.291%	
MMS4	Aug 10 2018 09:08:46.951	84264.667	84259.701	84259.786	-4.965	-4.881	-0.08436	1.699%	4.411%	
 
MMS2 was 0.18 m/s (net delta-v) and 11.99% axial, MMS3 was 0.065 m/s and 27.83% axial, and MMS4 was 0.12 m/s and 30.72% axial.

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.
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_FM912	2018_220/07:06:12 to 2018_220/07:06:22	0.0518	-0.1092	0.0146	
		0.01	0.01	0.01	
		-0.001561	0.002774	0.000681	
MMS3_FM912	2018_220/08:41:12 to 2018_220/08:41:12*	-0.026	-0.0377	-0.0455	
		0.01	0.01	0.01	
		-0.00601	0.007809	0.0008202	
MMS2_FM912	2018_220/11:51:12 to 2018_220/11:51:22	-0.0285	-0.154	-0.0827	
		0.01	0.01	0.01	
		-0.0007024	0.002492	0.0006617