FM897

Looking at the Restart states from Rev 898 we have the following results for FM897
FM897		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	Jun 29 2018 02:52:18.293	84276.726	84276.726	84276.756	0.000	0.030	-0.03003			
MMS2	Jun 29 2018 02:52:16.704	84276.761	84275.847	84275.853	-0.914	-0.908	-0.00559	0.612%	-1.500%	
MMS3	Jun 29 2018 02:52:55.757	84276.831	84278.696	84278.668	1.864	1.837	0.02756	1.478%	-1.179%	
MMS4	Jun 29 2018 02:52:52.145	84276.737	84275.970	84275.921	-0.767	-0.817	0.04968	-6.478%	-1.631%	
 
MMS2 was 0.22 m/s (net delta-v) and 19.64% axial, MMS3 was 0.16 m/s and 28.51% axial, and MMS4 was 0.10 m/s and 26.95% 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 except MMS4 DVX & DVY, and MMS3 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)	
MMS3_FM897	2018_178/08:21:12 to 2018_178/08:21:22	-0.1381	-0.0276	-0.0741	
		0.01	0.01	0.01	
		-0.008625	0.01018	0.000431	
MMS2_FM897	2018_178/09:56:12 to 2018_178/09:56:32	-0.1795	-0.0987	-0.0898	
		0.01	0.01	0.01	
		-0.007517	0.008457	0.000383	
MMS4_FM897	2018_178/11:31:12 to 2018_178/11:31:22	-0.0645	-0.048	-0.0615	
		0.01	0.01	0.01	
		-0.01655	0.0137	-0.0004409