FM790

Looking at the Restart states from Rev 791 we have the following results for FM790.
FM790		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	Aug 31 2017 22:24:06.805	83947.245	83944.490	83944.607	-2.755	-2.639	-0.11667	4.234%	5.277%	
MMS2	Aug 31 2017 22:24:14.053	83947.239	83948.104	83948.201	0.865	0.961	-0.09669	-11.182%	1.101%	
MMS3	Aug 31 2017 22:24:04.742	83947.246	83947.636	83947.692	0.391	0.446	-0.05528	-14.151%	2.901%	
MMS4	Aug 31 2017 22:23:59.257	83947.257	83947.257	83947.281	0.000	0.025	-0.02460			
 
MMS1 was 0.10 m/s (net delta-v) and 6.89% axial, MMS2 was 0.16 m/s and 65.96% axial, and MMS3 was 0.08 m/s and 15.30% axial. 
Larger SMA % errors due to small size of the maneuver.  Error in terms of meters is in line with FR753 and FR768, but smaller maneuvers.

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)	
MMS3_FM790	2017_242/01:16:12 to 2017_242/01:16:22	-0.0955	0.0006	0.0111	
		0.01	0.01	0.01	
		0.002455	-0.00366	-0.00007259	
MMS1_FM790	2017_242/05:01:12 to 2017_242/05:01:22	-0.1	-0.0609	-0.0257	
		0.01	0.01	0.01	
		0.001617	-0.0007356	0.00008529	
MMS2_FM790	2017_242/06:36:12 to 2017_242/06:36:42	-0.0808	-0.0268	0.1373	
		0.01	0.01	0.01	
		0.001151	0.0007623	0.0008821