FM434

Looking at the Restart states from Rev 435 we have the following results for FM434.
FM434		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	SMA error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)		
MMS1	May 19 2016 11:02:47.131	42106.460	42100.873	42100.887	-5.58667	-5.57296	-0.01371	0.25%	
MMS2	May 19 2016 11:02:49.339	42106.455	42106.455	42106.477	0.00000	0.02200	-0.02200		
MMS3	May 19 2016 11:02:15.919	42106.466	42102.706	42102.706	-3.76004	-3.76019	0.00015	0.00%	
MMS4	May 19 2016 11:02:24.835	42106.449	42104.361	42104.364	-2.08827	-2.08550	-0.00277	0.13%	

All three DVs were more radial this time.
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)	
MMS1_FM434	2016_139/15:21:11 to 2016_139/15:21:51	-0.4176	-0.1457	-0.1793	
		0.01	0.01	0.01	
		0.000419	-0.0003533	0.000116	
MMS3_FM434	2016_139/16:56:11 to 2016_139/16:56:51	-0.267	0.0045	-0.229	
		0.01	0.01	0.01	
		0.0005464	0.0002858	0.0004206	
MMS4_FM434	2016_139/18:31:11 to 2016_139/18:31:41	-0.3735	0.1085	-0.1311	
		0.01	0.01	0.01	
		0.0004477	0.001226	0.000848