FM407

Looking at the Restart states from Rev 408 we have the following results for FM407.
FM407		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	SMA error	PC error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)			
MMS1	Apr 22 2016 14:08:00.804	42100.828	42104.777	42104.756	3.94976	3.92884	0.02092	0.53%	0.36%	
MMS2	Apr 22 2016 14:07:53.491	42104.434	42104.773	42104.741	0.33936	0.30708	0.03228	9.51%	0.44%	
MMS3	Apr 22 2016 14:07:25.916	42104.775	42104.790	42104.764	0.01517	-0.01067	0.02585			
MMS4	Apr 22 2016 14:07:34.415	42104.697	42104.761	42104.744	0.06346	0.04655	0.01691	26.65%	0.19%	

All three DVs were highly axial so the Plane Change errors are the relevant values.  As seen above the “SMA error” (Plan – OD) in km for the reference spacecraft of the same magnitude of the other spacecraft.
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 for DVY which is basically at the requirement value.
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_FM407	2016_112/11:52:36 to 2016_112/11:54:36	-0.4247	-0.2692	-0.7805	
		0.004247	0.002692	0.007805	
		-0.0003838	-0.0004654	-0.0002684	
MMS1_FM407	2016_112/13:28:06 to 2016_112/13:29:36	0.0795	-0.8856	-0.7576	
		0.003	0.008856	0.007576	
		-0.001142	-0.001435	-0.0007468	
MMS4_FM407	2016_112/15:03:16 to 2016_112/15:04:36	0.0578	0.1996	-0.4101	
		0.002	0.002	0.004101	
		-0.0007394	-0.002033	-0.002167