One Week | Three Month | One Year | Five Year | Full Range | Min | Mean | Max |
---|
Delta/Yr below is a slope of the liear 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 | Mean | RMS | Delta/Yr | Delta/Yr/Yr | Unit | Description | Limit Violation | |
---|---|---|---|---|---|---|---|---|
ai1ax1x | on | -9.936e-04 | 4.103e-04 | -0.01 +/- 0.17 | -(1.18+/-1.90)e-4 | DEG/S | IRU-1 AXIS 1X ANALOG RATE | No Violation | off | -0.004 | 4.663e-04 | -3.88 +/- 0.24 | (5.99+/-12.22)e-4 | No Violation |
ai1ax1y | on | -0.001 | 4.121e-04 | -0.01 +/- 0.17 | -(1.30+/-15.97)e-5 | DEG/S | IRU-1 AXIS 1Y ANALOG RATE | No Violation | off | -0.005 | 4.691e-04 | -3.91 +/- 0.24 | -(5.62+/-88.75)e-5 | No Violation |
ai1ax2x | on | -5.230e-04 | 4.112e-04 | -0.01 +/- 0.17 | (8.69+/-28.06)e-5 | DEG/S | IRU-1 AXIS 2X ANALOG RATE | No Violation | off | -0.005 | 4.671e-04 | -3.88 +/- 0.24 | (3.97+/-11.64)e-4 | No Violation |
ai1ax2y | on | -5.095e-04 | 4.131e-04 | -0.01 +/- 0.17 | (9.36+/-21.49)e-5 | DEG/S | IRU-1 AXIS 2Y ANALOG RATE | No Violation | off | -0.005 | 4.684e-04 | -3.90 +/- 0.24 | (1.91+/-9.21)e-4 | No Violation |
ai2ax1x | on | 0.001 | 2.837e-04 | -0.01 +/- 0.15 | (4.77+/-17.84)e-5 | DEG/S | IRU-2 AXIS 1X ANALOG RATE | No Violation | off | 0.004 | 0.003 | -3.72 +/- 0.21 | -(5.27+/-160.20)e-4 | No Violation |
ai2ax1y | on | 0.001 | 2.866e-04 | -0.01 +/- 0.15 | (1.94+/-17.79)e-5 | DEG/S | IRU-2 AXIS 1Y ANALOG RATE | No Violation | off | 6.649e-04 | 0.003 | -3.72 +/- 0.21 | -0.00 +/- 0.02 | No Violation |
ai2ax2x | on | 0.001 | 2.857e-04 | -0.01 +/- 0.15 | (3.86+/-19.80)e-5 | DEG/S | IRU-2 AXIS 2X ANALOG RATE | No Violation | off | 0.002 | 0.003 | -3.72 +/- 0.21 | -0.00 +/- 0.01 | No Violation |
ai2ax2y | on | 0.001 | 2.865e-04 | -0.01 +/- 0.15 | -(6.50+/-13.89)e-5 | DEG/S | IRU-2 AXIS 2Y ANALOG RATE | No Violation | off | 9.068e-04 | 0.003 | -3.72 +/- 0.21 | -0.00 +/- 0.02 | No Violation |
aoalpang | -0.496 | 0.020 | -12.84 +/- 13.99 | 0.32 +/- 0.45 | DEG | FSS ALPHA ANGLE MEAS | No Violation | |
aoattqt1 | -5.013e-04 | 5.278e-04 | 0.03 +/- 0.36 | -0.00 +/- 0.01 | na | ESTIMATED SPACECRAFT ATTITUDE QUATERION 1 (ECI) | No Violation | |
aoattqt2 | -0.002 | 5.920e-04 | -0.03 +/- 0.41 | 0.01 +/- 0.01 | na | ESTIMATED SPACECRAFT ATTITUDE QUATERION 2 (ECI) | No Violation | |
aoattqt3 | -0.002 | 5.299e-04 | -0.04 +/- 0.37 | 0.01 +/- 0.01 | na | ESTIMATED SPACECRAFT ATTITUDE QUATERION 3 (ECI) | No Violation | |
aoattqt4 | -7.266e-04 | 2.686e-04 | 0.42 +/- 0.19 | 0.01 +/- 0.01 | na | ESTIMATED SPACECRAFT ATTITUDE QUATERION 4 (ECI) | No Violation | |
aobetang | -0.176 | 0.031 | -16.90 +/- 21.44 | 0.21 +/- 0.68 | DEG | FSS BETA ANGLE MEAS | No Violation | |
aocmdqt1 | -369.418 | 782.522 | (5.79+/-541.00)e3 | -0.01 +/- 0.01 | na | COMMANDED SPACECRAFT ATTITUDE QUATERNION 1 | No Violation | |
aocmdqt2 | -0.002 | 5.917e-04 | -0.03 +/- 0.41 | 0.01 +/- 0.01 | na | COMMANDED SPACECRAFT ATTITUDE QUATERNION 2 | No Violation | |
aocmdqt3 | -853.243 | 487.872 | (3.49+/-337.40)e3 | (1.58+/-131.80)e-4 | na | COMMANDED SPACECRAFT ATTITUDE QUATERNION 3 | No Violation | |
aoscpos1 | 1.770e+03 | 41.966 | (6.88+/-316.60)e2 | (5.95+/-1.70)e2 | KM | SPACECRAFT POSITION VECTOR X (ECI FRAME) | No Violation | |
aoscpos2 | -102.253 | 72.182 | -(3.27+/-4.99)e4 | -(1.34+/-0.26)e3 | KM | SPACECRAFT POSITION VECTOR Y (ECI FRAME) | No Violation | |
aoscpos3 | 1.063e+03 | 50.215 | (6.85+/-3.56)e4 | (2.42+/-2.22)e2 | KM | SPACECRAFT POSITION VECTOR Z (ECI FRAME) | No Violation | |
aoscvel1 | -4.689e-04 | 8.478e-04 | -0.00 +/- 0.59 | 0.01 +/- 0.01 | KMPS | SPACECRAFT VELOCITY VECTOR X ECI FRAME) | No Violation | |
aoscvel2 | 0.002 | 0.001 | 0.01 +/- 0.88 | -0.01 +/- 0.01 | KMPS | SPACECRAFT VELOCITY VECTOR Y (ECI FRAME) | No Violation | |
aoscvel3 | -0.001 | 0.001 | -0.01 +/- 0.89 | 0.02 +/- 0.01 | KMPS | SPACECRAFT VELOCITY VECTOR Z (ECI FRAME) | No Violation | |
aosunec1 | 0.003 | 0.001 | (3.96+/-7060.00)e-4 | -0.02 +/- 0.01 | na | UNIT VECTOR FROM THE SPACECRAFT TO THE SUN X (ECI FRAME) | No Violation | |
aosunec2 | 0.003 | 9.377e-04 | 0.02 +/- 0.65 | 0.02 +/- 0.01 | na | UNIT VECTOR FROM THE SPACECRAFT TO THE SUN Y (ECI FRAME) | No Violation | |
aosunec3 | 0.001 | 4.067e-04 | 0.01 +/- 0.28 | 0.01 +/- 0.00 | na | UNIT VECTOR FROM THE SPACECRAFT TO THE SUN Z (ECI FRAME) | No Violation | |
aosunsa1 | -2.328e-04 | 1.296e-05 | -0.00 +/- 0.01 | -(1.86+/-1.50)e-4 | na | CSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME X | No Violation | |
aosunsa2 | 2.403e-04 | 2.349e-05 | 0.00 +/- 0.02 | -(8.86+/-47.56)e-5 | na | CSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME Y | No Violation | |
aosunsa3 | 7.488e-07 | 7.940e-06 | -1.00 +/- 0.01 | (1.44+/-32.82)e-6 | na | CSSA DERIVED UNIT VECTOR TO THE SUN IN SA FRAME Z | No Violation | |
aotarqt1 | -4.712e-04 | 5.268e-04 | 0.03 +/- 0.36 | -0.00 +/- 0.01 | na | TARGET ATTITUDE QUATERNION ELEMENT 1 | No Violation | |
aotarqt2 | -0.002 | 5.906e-04 | -0.03 +/- 0.41 | 0.01 +/- 0.01 | na | TARGET ATTITUDE QUATERNION ELEMENT 2 | No Violation | |
aotarqt3 | -0.002 | 5.289e-04 | -0.04 +/- 0.37 | 0.01 +/- 0.01 | na | TARGET ATTITUDE QUATERNION ELEMENT 3 | No Violation |
If you have any questions, please contact
swolk@cfa.harvard.edu.
Data Updated: Aug 10, 2023
Last Site Modification: Sep 30, 2021