FR216

Looking at the Restart states from Rev 217 we have the following results for FR216. 

FR202		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	Oct 15 2015 12:01:03.255	42112.843	42117.035	42117.026	4.192	4.183	-0.00876	-0.21%	
MMS2	Oct 15 2015 12:00:29.832	42112.829	42102.351	42102.354	-10.478	-10.475	0.00319	-0.03%	
MMS3	Oct 15 2015 12:01:07.052	42112.821	42112.821	42112.824	0.000	0.003	0.00306		
MMS4	Oct 15 2015 12:01:13.972	42112.843	42102.830	42102.804	-10.013	-10.039	-0.02587	0.26%	

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 maneuver planning requirements for 1/ 2 orbit predictions for FR216
•	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 2 days prior to the maneuver for FR216 vs the definitive GEONS state at the time of the maneuver.
The predicted velocity differences at the time of each maneuver are less than the greater of 1% of the delta-V or 10 mm/s for the first maneuver with significant margin.
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_FR216	287/03:40:35– 287/03:42:45	1.40666	-0.85350	0.154369	
		0.014	0.010	0.010	
		0.003	0.003	0.002	
MMS4_FR216	287/14:35:35- 287/14:38:35	-0.64326	-2.244342	-0.011857	
		0.010	0.022	0.010	
		0.002	0.002	0.0005	
MMS2_FR216	287/16:10:35- 287/16:11:45	-0.866893	-0.162786	-0.099692	
		0.010	0.010	0.010	
		0.002	0.0012	0.0005	

All FR216 maneuvers were planned using predicted ephemeris files based on GEONS post-perigee RST vectors @ 2015-285/02:56, one day prior to the CAM.  Note that these predictions start 2+ orbits prior to FR216.  Because the FR216 maneuvers started only a couple of hours post-perigee,  the CAM was held the prior day and final maneuver plans had to be prepared prior to the CAM.