FM343

Looking at the Restart states from Rev 344 we have the following results for FM343.

FM343		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 18 2016 21:40:44.275	42101.535	42097.628	42097.606	-3.907	-3.928	0.02191	-0.56%	
MMS2	Feb 18 2016 21:40:58.935	42101.544	42103.823	42103.805	2.279	2.260	0.01879	0.82%	
MMS3	Feb 18 2016 21:40:40.225	42101.530	42100.706	42100.689	-0.824	-0.841	0.01698	-2.06%	
MMS4	Feb 18 2016 21:40:48.890	42101.514	42101.514	42101.518	0.000	0.004	-0.00398		

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

FM343	Plan Change Plan	Plan Change OD	error	
MMS3	0.00324	0.00327	0.86%	

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_FM343	49/04:06:10 - 49/04:06:30	-0.2347	-0.1074	-0.0523	
		0.01	0.01	0.01	
		0.0002	0.0015	0.001	
MMS2_FM343	49/05:16:10 - 49/05:16:30	-0.2071	0.1702	0.1673	
		0.01	0.01	0.01	
		0.0011	0.0021	0.0012	
MMS3_FM343	49/06:41:10 -49/06:41:10	0.0163	0.0149	-0.1022	
		0.01	0.01	0.01	
		-0.0015	0.0035	0.002