Back to Top

PCADGRATE
Static Version: Max --- One Week

One Week Three Month One Year Five Year Full Range Min Mean Max

Delta/Yr below is a slope of the linear fitting over the data of the period. Delta/Yr/Yr is a slope of the liner fitting over the devivative data of the period. Slope listed on a linked plot is the slope computed on the last few periods of the data to show the direction of the trend, and different from that of Delta/Yr.

MSID MeanRMSDelta/YrDelta/Yr/YrUnitDescriptionLimit Violation
ai1ax1xon-0.0020.103-0.91 +/- 1.58(2.37+/-2.22)e2DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off7.965e-042.400e-04-3.85 +/- 0.02-0.69 +/- 1.67No Violation Check
ai1ax1yon-0.0010.104-0.92 +/- 1.60(2.31+/-2.24)e2DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off6.787e-042.078e-04-3.89 +/- 0.02-1.93 +/- 1.39No Violation Check
ai1ax2xon-0.0040.104-0.92 +/- 1.60(2.35+/-2.24)e2DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off-1.285e-041.462e-04-3.88 +/- 0.01-0.26 +/- 0.79No Violation Check
ai1ax2yon-0.0010.104-0.92 +/- 1.60(2.34+/-2.24)e2DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off-1.103e-041.493e-04-3.88 +/- 0.010.10 +/- 0.84No Violation Check
ai2ax1xon1.126e-041.591e-04(2.83+/-150.00)e-4-0.01 +/- 1.73DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-2.4240.063-1.49 +/- 1.78-17.74 +/- 46.48No Violation Check
ai2ax1yon-1.001e-041.012e-04(4.15+/-90.00)e-4-0.15 +/- 0.84DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-2.5140.066-1.54 +/- 1.85-26.72 +/- 47.61No Violation Check
ai2ax2xon5.314e-051.532e-04(4.88+/-140.00)e-40.90 +/- 1.67DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-2.4870.065-1.53 +/- 1.83-26.77 +/- 47.14No Violation Check
ai2ax2yon5.013e-059.220e-05(3.42+/-900.00)e-50.03 +/- 0.71DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-2.5310.066-1.53 +/- 1.86-30.24 +/- 47.83No Violation Check
aoalpang 0.0620.246-8.62 +/- 22.85(1.61+/-2.46)e3DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 0.0190.003-0.04 +/- 0.27-13.84 +/- 14.97naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 0.0130.005-0.54 +/- 0.4531.21 +/- 31.35naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 -0.0020.0030.12 +/- 0.2920.03 +/- 12.79naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 6.937e-050.0030.47 +/- 0.3232.88 +/- 34.25naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang -1.0590.3971.07 +/- 36.96(2.34+/-3.65)e3DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 0.0190.003-0.04 +/- 0.27-13.95 +/- 14.96naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 0.0140.005-0.54 +/- 0.4536.74 +/- 31.70naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 -0.0020.0030.12 +/- 0.2919.91 +/- 12.81naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 1.109e+03256.752-(3.67+/-23.55)e3-(1.11+/-0.36)e6KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 2.762e+03443.342-(7.77+/-4.09)e4(2.78+/-0.69)e6KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 -3.280e+03381.596(5.80+/-3.55)e4-(3.91+/-5.78)e5KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 -0.0660.0110.00 +/- 0.99-71.75 +/- 32.97KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 0.0970.0170.18 +/- 1.54-5.68 +/- 35.09KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 0.0190.014-0.10 +/- 1.3271.60 +/- 31.29KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 -0.0043.195e-050.97 +/- 0.01-0.02 +/- 0.03naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 0.0153.131e-050.23 +/- 0.03-0.05 +/- 0.19naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 0.0073.081e-050.10 +/- 0.010.01 +/- 0.05naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 2.132e-041.057e-04-0.01 +/- 0.010.13 +/- 0.82naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 -0.0012.676e-040.01 +/- 0.03-0.61 +/- 2.14naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 -7.363e-051.973e-05-1.00 +/- 0.00-0.05 +/- 0.12naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 0.0150.003-0.04 +/- 0.27-18.53 +/- 14.94naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.0190.005-0.52 +/- 0.4825.06 +/- 33.38naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 -4.524e-040.0030.11 +/- 0.3017.09 +/- 12.84naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

If you have any questions, please contact swolk@cfa.harvard.edu.

Data Updated: Apr 09, 2026
Last Site Modification: Sep 30, 2021