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SatNOGS Orbit Determination
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SatNOGS Orbit Determination
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7802b2f9
Commit
7802b2f9
authored
5 years ago
by
Luc Maisonobe
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Tuned input parameter so OD converges.
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004d5622
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src/main/resources/maxvalier.in
+7
-7
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src/main/resources/maxvalier.in
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src/main/resources/maxvalier.in
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7802b2f9
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@@ -69,17 +69,17 @@ orbit.date = 2019-06-11T16:35:29.149
### Cartesian elements
## Position along X in inertial frame (m)
orbit.cartesian.px = -5
4
23194
orbit.cartesian.px = -52
7
3194
## Position along Y in inertial frame (m)
orbit.cartesian.py = -4
5
50295
orbit.cartesian.py = -4
4
50295
## Position along Z in inertial frame (m)
orbit.cartesian.pz =
25
0075
orbit.cartesian.pz =
11
0075
## Velocity along X in inertial frame (m/s)
orbit.cartesian.vx = -
73
5
orbit.cartesian.vx = -
58
5
## Velocity along Y in inertial frame (m/s)
orbit.cartesian.vy = 7
4
0
orbit.cartesian.vy = 7
9
0
## Velocity along Z in inertial frame (m/s)
orbit.cartesian.vz = 7
7
60
orbit.cartesian.vz = 76
1
0
## TLE parameters
#Line 1
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@@ -272,7 +272,7 @@ estimator.optimization.engine = Levenberg-Marquardt
# divided by estimator.orbital.parameters.position.scale. So if the initial guess
# is about 100km wrong and estimator.orbital.parameters.position.scale is set to 10.0,
# the initial step bound factor should be of the order of magnitude of 1.0e6
estimator.Levenberg.Marquardt.initial.step.bound.factor = 1.0
e6
estimator.Levenberg.Marquardt.initial.step.bound.factor = 1
00
.0
# convergence is reached when max|p(k+1) - p(k)| < ε for each
# normalized estimated parameters p and iterations k and k+1
...
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