FR282 & FR283

Looking at the Restart states from Rev 283 and Rev 284, we have the following results for FR282 and FR283 respectively.  These are the MMS4 burns that were not done on FR279 & FR280.  The burn was mostly out of plane, so the nominal calculations of SMA change less illuminating. So, we have made a plane change calculation and present those results

FR282	Epoch of Plan Apogee	Plan Change Plan	Plan Change OD	error	
MMS4	Dec 20 2015 04:46:23.151	0.0382603	0.0383024	0.11%	
FR283	Epoch of Plan Apogee	Plan Change Plan	Plan Change OD	error	
MMS4	Dec 21 2015 04:39:43.705	0.0250503	0.0250320	-0.07%	

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)	
MMS4_FR282	353/12:50:35-353/12:53:35	-0.011517	-0.49748	0.8389	
		0.01	0.01	0.01	
		0.0005	0.0015	0.0004	
MMS4_FR283	354/03:32:40-354/03:34:00	-0.062157	0.00374	-0.48692	
		0.002	0.002	0.0048692	
		0.001	0.001	0.0005