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update: some docs and cleanups
1 parent cb84a82 commit 134528f

23 files changed

Lines changed: 2475 additions & 120 deletions

‎docs/notebooks/cdms_analysis_and_plotting.ipynb‎

Lines changed: 37 additions & 35 deletions
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‎docs/notebooks/plotting.ipynb‎

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‎docs/notebooks/probabilistic_programming_module.ipynb‎

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‎docs/notebooks/synthetic_cdms/event1_0.kvn‎

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CCSDS_CDM_VERS = 1.0
2+
CREATION_DATE = 2025-02-21T03:20:45.423178
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ORIGINATOR = KESSLER_SOFTWARE
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MESSAGE_ID = KESSLER_SOFTWARE_0487ea22-138a-11f0-a1a9-f2a9f71f7e19
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TCA = 2025-02-23T16:41:51.264217
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MISS_DISTANCE = 1599.385783304641
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RELATIVE_SPEED = 8.406610360741997
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RELATIVE_POSITION_R = -200.339469550585
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RELATIVE_POSITION_T = -58.25940943259976
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RELATIVE_POSITION_N = 1585.7190236576453
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RELATIVE_VELOCITY_R = -1.6575886604725651
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RELATIVE_VELOCITY_T = -4.702562654172012
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RELATIVE_VELOCITY_N = 6.768264332426308
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COLLISION_PROBABILITY = 0.0
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COLLISION_PROBABILITY_METHOD = MC
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OBJECT = OBJECT1
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OBJECT_DESIGNATOR = 76126AP
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CATALOG_NAME = 9827
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OBJECT_NAME = COSMOS 886 DEB
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INTERNATIONAL_DESIGNATOR = 76126AP
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EPHEMERIS_NAME = NONE
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COVARIANCE_METHOD = CALCULATED
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MANEUVERABLE = N/A
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ORBIT_CENTER = EARTH
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REF_FRAME = ITRF
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Y = -1354.1077713033583
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Y_DOT = 7.152468300076865
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Z_DOT = -0.8184870561932284
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CR_R = 0.15212996364233536
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CT_R = 1.767066619611639
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CT_T = 61.13843097922123
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CN_R = -0.00022143993045502212
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CN_T = -0.002137168496384415
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CN_N = 5.538E-07
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CRDOT_R = -0.001387624846756269
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CRDOT_T = -0.059321445102163514
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CRDOT_N = 1.253E-06
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CRDOT_RDOT = 5.902E-05
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CTDOT_R = -0.00016387167746678447
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CTDOT_T = -0.0016034103637458102
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CTDOT_N = 2.467E-07
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CTDOT_RDOT = 1.169E-06
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CTDOT_TDOT = 1.788E-07
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CNDOT_R = 4.418E-06
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CNDOT_T = 9.513E-05
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CNDOT_N = -8.329E-09
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CNDOT_RDOT = -8.374E-08
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CNDOT_TDOT = -4.487E-09
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CNDOT_NDOT = 2.003E-10
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OBJECT = OBJECT2
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OBJECT_DESIGNATOR = 69082CJ
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CATALOG_NAME = 4227
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OBJECT_NAME = THORAD AGENA D DEB
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INTERNATIONAL_DESIGNATOR = 69082CJ
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EPHEMERIS_NAME = NONE
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COVARIANCE_METHOD = CALCULATED
60+
MANEUVERABLE = N/A
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ORBIT_CENTER = EARTH
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REF_FRAME = ITRF
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X = 3862.163156007167
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Y = -1686.8001744420503
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Z = -5334.255177107932
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X_DOT = 6.152228410666328
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Y_DOT = 1.618574029450763
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Z_DOT = 3.9415013431369377
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CR_R = 3.852952621853669
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CT_R = 0.0
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CT_T = 4.976328968225473
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CN_R = 0.0
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CN_T = 0.0
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CN_N = 0.9333314012997196
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CRDOT_R = 0.0
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CRDOT_T = 0.0
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CRDOT_N = 0.0
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CRDOT_RDOT = 1.000E-18
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CTDOT_R = 0.0
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CTDOT_T = 0.0
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CTDOT_N = 0.0
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CTDOT_RDOT = 0.0
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CTDOT_TDOT = 1.000E-18
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CNDOT_R = 0.0
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CNDOT_T = 0.0
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CNDOT_N = 0.0
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CNDOT_RDOT = 0.0
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CNDOT_TDOT = 0.0
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CNDOT_NDOT = 1.000E-18

‎docs/notebooks/synthetic_cdms/event1_1.kvn‎

Lines changed: 89 additions & 0 deletions
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CCSDS_CDM_VERS = 1.0
2+
CREATION_DATE = 2025-02-21T11:21:54.534947
3+
ORIGINATOR = KESSLER_SOFTWARE
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MESSAGE_ID = KESSLER_SOFTWARE_065dc20e-138a-11f0-a1a9-f2a9f71f7e19
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TCA = 2025-02-23T16:41:51.264217
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MISS_DISTANCE = 1348.1981020987255
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RELATIVE_SPEED = 8.426512407592309
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RELATIVE_POSITION_R = -144.82803645001906
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RELATIVE_POSITION_T = -37.32697360897995
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RELATIVE_POSITION_N = 1339.8767329130812
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RELATIVE_VELOCITY_R = -1.4171204689506622
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RELATIVE_VELOCITY_T = -4.728716409300112
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RELATIVE_VELOCITY_N = 6.829137723915373
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COLLISION_PROBABILITY = 0.0
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COLLISION_PROBABILITY_METHOD = MC
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OBJECT = OBJECT1
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OBJECT_DESIGNATOR = 76126AP
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CATALOG_NAME = 9827
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OBJECT_NAME = COSMOS 886 DEB
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INTERNATIONAL_DESIGNATOR = 76126AP
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EPHEMERIS_NAME = NONE
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COVARIANCE_METHOD = CALCULATED
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MANEUVERABLE = N/A
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ORBIT_CENTER = EARTH
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REF_FRAME = ITRF
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X_DOT = 2.026748694780936
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Y_DOT = 7.123981881789366
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Z_DOT = -0.9557733246802299
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CR_R = 1.000E-18
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CT_R = 0.0
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CT_T = 1.2451197530695846
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CN_R = 0.0
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CN_T = 0.0
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CN_N = 0.0035176566277315556
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CRDOT_R = 0.0
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CRDOT_T = 0.0
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CRDOT_N = 0.0
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CRDOT_RDOT = 1.000E-18
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CTDOT_R = 0.0
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CTDOT_T = 0.0
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CTDOT_N = 0.0
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CTDOT_RDOT = 0.0
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CTDOT_TDOT = 1.000E-18
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CNDOT_R = 0.0
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CNDOT_T = 0.0
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CNDOT_N = 0.0
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CNDOT_RDOT = 0.0
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CNDOT_TDOT = 0.0
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CNDOT_NDOT = 1.000E-18
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OBJECT = OBJECT2
54+
OBJECT_DESIGNATOR = 69082CJ
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CATALOG_NAME = 4227
56+
OBJECT_NAME = THORAD AGENA D DEB
57+
INTERNATIONAL_DESIGNATOR = 69082CJ
58+
EPHEMERIS_NAME = NONE
59+
COVARIANCE_METHOD = CALCULATED
60+
MANEUVERABLE = N/A
61+
ORBIT_CENTER = EARTH
62+
REF_FRAME = ITRF
63+
X = 3633.97930307704
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Y = -1752.8652636247746
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Z = -5472.2177740416755
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X_DOT = 6.3158434028298185
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Y_DOT = 1.5594194830663326
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Z_DOT = 3.696690888122699
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CR_R = 3.852952621853669
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CT_R = 0.0
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CT_T = 4.976328968225473
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CN_R = 0.0
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CN_T = 0.0
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CN_N = 0.9333314012997196
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CRDOT_R = 0.0
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CRDOT_T = 0.0
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CRDOT_N = 0.0
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CRDOT_RDOT = 1.000E-18
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CTDOT_R = 0.0
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CTDOT_T = 0.0
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CTDOT_N = 0.0
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CTDOT_RDOT = 0.0
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CTDOT_TDOT = 1.000E-18
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CNDOT_R = 0.0
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CNDOT_T = 0.0
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CNDOT_N = 0.0
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CNDOT_RDOT = 0.0
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CNDOT_TDOT = 0.0
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CNDOT_NDOT = 1.000E-18

‎docs/notebooks/synthetic_cdms/event1_2.kvn‎

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CCSDS_CDM_VERS = 1.0
2+
CREATION_DATE = 2025-02-21T19:23:27.838699
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ORIGINATOR = KESSLER_SOFTWARE
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MESSAGE_ID = KESSLER_SOFTWARE_08026d94-138a-11f0-a1a9-f2a9f71f7e19
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TCA = 2025-02-23T16:41:51.264217
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MISS_DISTANCE = 1350.0796621043116
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RELATIVE_SPEED = 8.454050021758691
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RELATIVE_POSITION_R = -144.81703693484633
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RELATIVE_POSITION_T = 67.94727738222727
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RELATIVE_POSITION_N = 1340.5693892288627
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RELATIVE_VELOCITY_R = -1.4604528250723996
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RELATIVE_VELOCITY_T = -4.759987253763458
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RELATIVE_VELOCITY_N = 6.832317371152016
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COLLISION_PROBABILITY = 0.0
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COLLISION_PROBABILITY_METHOD = MC
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OBJECT = OBJECT1
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OBJECT_DESIGNATOR = 76126AP
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CATALOG_NAME = 9827
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OBJECT_NAME = COSMOS 886 DEB
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INTERNATIONAL_DESIGNATOR = 76126AP
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EPHEMERIS_NAME = NONE
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COVARIANCE_METHOD = CALCULATED
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MANEUVERABLE = N/A
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ORBIT_CENTER = EARTH
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REF_FRAME = ITRF
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X_DOT = 2.0620055705717224
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Y_DOT = 7.098892719307384
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Z_DOT = -1.066717737243908
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CR_R = 1.000E-18
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CT_R = 0.0
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CT_T = 1.2451197530695846
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CN_R = 0.0
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CN_T = 0.0
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CN_N = 0.0035176566277315556
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CRDOT_R = 0.0
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CRDOT_T = 0.0
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CRDOT_N = 0.0
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CRDOT_RDOT = 1.000E-18
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CTDOT_R = 0.0
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CTDOT_T = 0.0
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CTDOT_N = 0.0
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CTDOT_RDOT = 0.0
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CTDOT_TDOT = 1.000E-18
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CNDOT_R = 0.0
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CNDOT_T = 0.0
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CNDOT_N = 0.0
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CNDOT_RDOT = 0.0
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CNDOT_TDOT = 0.0
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CNDOT_NDOT = 1.000E-18
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OBJECT = OBJECT2
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OBJECT_DESIGNATOR = 69082CJ
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CATALOG_NAME = 4227
56+
OBJECT_NAME = THORAD AGENA D DEB
57+
INTERNATIONAL_DESIGNATOR = 69082CJ
58+
EPHEMERIS_NAME = NONE
59+
COVARIANCE_METHOD = CALCULATED
60+
MANEUVERABLE = N/A
61+
ORBIT_CENTER = EARTH
62+
REF_FRAME = ITRF
63+
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Y = -1752.8652636247746
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Z = -5472.2177740416755
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X_DOT = 6.3158434028298185
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Y_DOT = 1.5594194830663326
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Z_DOT = 3.696690888122699
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CR_R = 3.852952621853669
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CT_R = 0.0
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CT_T = 4.976328968225473
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CN_R = 0.0
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CN_T = 0.0
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CN_N = 0.9333314012997196
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CRDOT_R = 0.0
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CRDOT_T = 0.0
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CRDOT_N = 0.0
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CRDOT_RDOT = 1.000E-18
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CTDOT_R = 0.0
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CTDOT_T = 0.0
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CTDOT_N = 0.0
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CTDOT_RDOT = 0.0
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CTDOT_TDOT = 1.000E-18
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CNDOT_R = 0.0
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CNDOT_T = 0.0
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CNDOT_N = 0.0
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CNDOT_RDOT = 0.0
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CNDOT_TDOT = 0.0
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CNDOT_NDOT = 1.000E-18

‎docs/notebooks/synthetic_cdms/event1_3.kvn‎

Lines changed: 89 additions & 0 deletions
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1+
CCSDS_CDM_VERS = 1.0
2+
CREATION_DATE = 2025-02-22T03:21:09.302550
3+
ORIGINATOR = KESSLER_SOFTWARE
4+
MESSAGE_ID = KESSLER_SOFTWARE_08db3ae8-138a-11f0-a1a9-f2a9f71f7e19
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TCA = 2025-02-23T16:41:51.264217
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MISS_DISTANCE = 1357.4019853542814
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RELATIVE_SPEED = 8.47595736838985
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RELATIVE_POSITION_R = -146.08669906273596
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RELATIVE_POSITION_T = 149.50290341697263
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RELATIVE_POSITION_N = 1341.2112839036936
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RELATIVE_VELOCITY_R = -1.493709934496736
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RELATIVE_VELOCITY_T = -4.7849122253265985
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RELATIVE_VELOCITY_N = 6.8348591015666145
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COLLISION_PROBABILITY = 0.0
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COLLISION_PROBABILITY_METHOD = MC
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OBJECT = OBJECT1
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OBJECT_DESIGNATOR = 76126AP
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CATALOG_NAME = 9827
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OBJECT_NAME = COSMOS 886 DEB
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INTERNATIONAL_DESIGNATOR = 76126AP
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EPHEMERIS_NAME = NONE
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COVARIANCE_METHOD = CALCULATED
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MANEUVERABLE = N/A
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ORBIT_CENTER = EARTH
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REF_FRAME = ITRF
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Z_DOT = -1.1526698586334423
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CR_R = 1.000E-18
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CT_R = 0.0
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CT_T = 1.2451197530695846
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CN_R = 0.0
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CN_T = 0.0
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CN_N = 0.0035176566277315556
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CRDOT_R = 0.0
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CRDOT_T = 0.0
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CRDOT_N = 0.0
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CRDOT_RDOT = 1.000E-18
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CTDOT_R = 0.0
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CTDOT_T = 0.0
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CTDOT_N = 0.0
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CTDOT_RDOT = 0.0
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CTDOT_TDOT = 1.000E-18
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CNDOT_R = 0.0
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CNDOT_T = 0.0
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CNDOT_N = 0.0
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CNDOT_RDOT = 0.0
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CNDOT_TDOT = 0.0
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CNDOT_NDOT = 1.000E-18
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OBJECT = OBJECT2
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OBJECT_DESIGNATOR = 69082CJ
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CATALOG_NAME = 4227
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OBJECT_NAME = THORAD AGENA D DEB
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INTERNATIONAL_DESIGNATOR = 69082CJ
58+
EPHEMERIS_NAME = NONE
59+
COVARIANCE_METHOD = CALCULATED
60+
MANEUVERABLE = N/A
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ORBIT_CENTER = EARTH
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REF_FRAME = ITRF
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Y = -1752.8652636247746
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Z = -5472.2177740416755
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X_DOT = 6.3158434028298185
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Y_DOT = 1.5594194830663326
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Z_DOT = 3.696690888122699
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CR_R = 3.852952621853669
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CT_R = 0.0
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CT_T = 4.976328968225473
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CN_R = 0.0
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CN_T = 0.0
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CN_N = 0.9333314012997196
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CRDOT_R = 0.0
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CRDOT_T = 0.0
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CRDOT_N = 0.0
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CRDOT_RDOT = 1.000E-18
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CTDOT_R = 0.0
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CTDOT_T = 0.0
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CTDOT_N = 0.0
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CTDOT_RDOT = 0.0
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CTDOT_TDOT = 1.000E-18
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CNDOT_R = 0.0
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CNDOT_T = 0.0
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CNDOT_N = 0.0
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CNDOT_RDOT = 0.0
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CNDOT_TDOT = 0.0
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CNDOT_NDOT = 1.000E-18

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