Back to Top

PCADGRATE
Static Version: Min --- 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
ai1ax1xon0.0050.105-0.96 +/- 1.60(1.86+/-1.94)e2DEG/SIRU-1 AXIS 1X ANALOG RATENo Violation Check
off4.575e-042.322e-04-3.90 +/- 0.02-0.65 +/- 1.51No Violation Check
ai1ax1yon0.0150.106-0.96 +/- 1.62(2.04+/-1.97)e2DEG/SIRU-1 AXIS 1Y ANALOG RATENo Violation Check
off-9.552e-061.305e-04-3.94 +/- 0.010.07 +/- 0.73No Violation Check
ai1ax2xon0.0010.106-0.94 +/- 1.62(1.93+/-1.97)e2DEG/SIRU-1 AXIS 2X ANALOG RATENo Violation Check
off7.725e-051.673e-04-3.91 +/- 0.010.17 +/- 0.95No Violation Check
ai1ax2yon0.0150.106-0.96 +/- 1.62(2.00+/-1.97)e2DEG/SIRU-1 AXIS 2Y ANALOG RATENo Violation Check
off-3.898e-051.255e-04-3.94 +/- 0.01-0.24 +/- 0.73No Violation Check
ai2ax1xon6.952e-051.795e-04-0.00 +/- 0.021.61 +/- 1.91DEG/SIRU-2 AXIS 1X ANALOG RATENo Violation Check
off-2.4320.064-1.53 +/- 1.79-50.59 +/- 87.65No Violation Check
ai2ax1yon5.679e-051.208e-04-0.00 +/- 0.010.13 +/- 1.12DEG/SIRU-2 AXIS 1Y ANALOG RATENo Violation Check
off-2.5350.066-1.56 +/- 1.86-58.68 +/- 90.54No Violation Check
ai2ax2xon-2.432e-041.969e-04-0.01 +/- 0.021.24 +/- 2.11DEG/SIRU-2 AXIS 2X ANALOG RATENo Violation Check
off-2.5160.066-1.55 +/- 1.85-55.90 +/- 89.76No Violation Check
ai2ax2yon1.698e-049.486e-05-0.00 +/- 0.010.47 +/- 0.81DEG/SIRU-2 AXIS 2Y ANALOG RATENo Violation Check
off-2.5200.066-1.56 +/- 1.85-59.77 +/- 90.71No Violation Check
aoalpang -0.7150.259-14.97 +/- 23.77-(5.92+/-25.67)e2DEGFSS ALPHA ANGLE MEASNo Violation Check
aoattqt1 0.0120.005-0.23 +/- 0.50-38.41 +/- 27.84naESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI)No Violation Check
aoattqt2 0.0090.0030.26 +/- 0.30-7.13 +/- 25.09naESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI)No Violation Check
aoattqt3 -0.0110.005-0.07 +/- 0.4737.56 +/- 28.73naESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI)No Violation Check
aoattqt4 0.0640.0020.50 +/- 0.25-11.17 +/- 15.21naESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI)No Violation Check
aobetang -1.5980.382-10.33 +/- 35.21(1.08+/-3.87)e3DEGFSS BETA ANGLE MEASNo Violation Check
aocmdqt1 0.0120.005-0.23 +/- 0.50-38.45 +/- 27.84naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 1No Violation Check
aocmdqt2 0.0090.0030.26 +/- 0.30-7.09 +/- 25.09naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 2No Violation Check
aocmdqt3 -0.0110.005-0.07 +/- 0.4737.58 +/- 28.73naCOMMANDED SPACECRAFT ATTITUDE QUATERNION 3No Violation Check
aoscpos1 -1.151e+03264.665-(1.43+/-2.38)e4(1.20+/-0.39)e6KMSPACECRAFT POSITION VECTOR X (ECI FRAME)No Violation Check
aoscpos2 -2.243e+03459.807-(6.45+/-4.15)e4-(2.53+/-0.76)e6KMSPACECRAFT POSITION VECTOR Y (ECI FRAME)No Violation Check
aoscpos3 3.114e+03428.636(6.09+/-3.89)e4-(7.24+/-6.54)e5KMSPACECRAFT POSITION VECTOR Z (ECI FRAME)No Violation Check
aoscvel1 0.0490.010-0.07 +/- 0.9434.51 +/- 31.35KMPSSPACECRAFT VELOCITY VECTOR X ECI FRAME)No Violation Check
aoscvel2 -0.0820.018-0.04 +/- 1.59-6.96 +/- 37.13KMPSSPACECRAFT VELOCITY VECTOR Y (ECI FRAME)No Violation Check
aoscvel3 -0.0170.0150.11 +/- 1.38-35.71 +/- 32.68KMPSSPACECRAFT VELOCITY VECTOR Z (ECI FRAME)No Violation Check
aosunec1 0.0073.260e-05-0.91 +/- 0.01-0.01 +/- 0.06naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME)No Violation Check
aosunec2 -0.0143.255e-05-0.38 +/- 0.030.15 +/- 0.17naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME)No Violation Check
aosunec3 -0.0063.269e-05-0.17 +/- 0.010.05 +/- 0.07naUNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME)No Violation Check
aosunsa1 0.0021.155e-04-0.01 +/- 0.010.87 +/- 1.01naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME XNo Violation Check
aosunsa2 -0.0023.052e-040.01 +/- 0.03-1.35 +/- 1.77naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME YNo Violation Check
aosunsa3 1.248e-051.671e-05-1.00 +/- 0.00-0.01 +/- 0.01naCSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME ZNo Violation Check
aotarqt1 0.0150.005-0.22 +/- 0.50-44.09 +/- 28.09naTARGET ATTITUDE QUATERNION ELEMENT 1No Violation Check
aotarqt2 0.0080.0030.26 +/- 0.31-8.32 +/- 25.43naTARGET ATTITUDE QUATERNION ELEMENT 2No Violation Check
aotarqt3 -0.0100.005-0.06 +/- 0.4750.47 +/- 29.28naTARGET ATTITUDE QUATERNION ELEMENT 3No Violation Check

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

Data Updated: Oct 23, 2026
Last Site Modification: Sep 30, 2021