FM344

Looking at the Restart states from Rev 345 we have the following results for FM344.

FM344		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)		
MMS1	Feb 19 2016 21:33:48.926	42097.080	42100.946	42100.974	3.866	3.894	-0.02819	-0.73%	
MMS2	Feb 19 2016 21:33:46.002	42103.274	42100.948	42100.955	-2.326	-2.319	-0.00731	0.31%	
MMS3	Feb 19 2016 21:33:35.965	42100.162	42100.950	42100.970	0.788	0.808	-0.02024	-2.57%	

MMS3 is more of a plane change maneuver (mostly axial) and the results relative to that are the following:

FM344	Plan Change Plan	Plan Change OD	error	
MMS3	0.00367	0.00369	0.61%	

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_FM344	49/18:03:45 - 49/18:04:35	-0.2765	-0.5181	-0.1964	
		0.002765	0.005181	0.002	
		-0.0005	-0.0004	-0.0033	
MMS2_FM344	49/19:39:15 - 49/19:39:35	-0.0477	0.2907	0.0984	
		0.002	0.002907	0.002	
		-0.001	-0.001	-0.0006	
MMS3_FM344	49/21:14:25 - 49/21:14:35	0.0241	-0.1963	-0.0327	
		0.002	0.002	0.002	
		-0.0015	-0.002	-0.00125