ParametrizationAcceleration

This class defines parameters of satellite accelerations. It will be used to set up the design matrix in a least squares adjustment. If multiple parametrizations are given the coefficients in the parameter vector are sequently appended.

PerRevolution

Oscillation once, twice, ... per revolution in Satellite Reference Frame (SRF) with the argument of latitude as input angle. If the attitude of the satellite is not provided the Celestial Reference Frame (CRF) is used instead. Paramters are estimated in $[nm/s^2=10^{-9}\,m/s^2]$.

The parameter names are

NameTypeAnnotation
order
uintonce, twice, ...
estimateX
booleanalong
estimateY
booleancross
estimateZ
booleanradial
interval
timeSeriessetup new parameters each interval
perArc
boolean

AccBias

Temporal changing accelerometer bias per axis in $[m/s^2]$ in Satellite Reference Frame (SRF). If the attitude of the satellite is not provided the Celestial Reference Frame (CRF) is used instead.

The parameter names are

NameTypeAnnotation
estimateX
booleanalong
estimateY
booleancross
estimateZ
booleanradial
temporal
parametrizationTemporal
perArc
boolean

AccelerometerScaleFactors

Accelerometer scale factor per axis.

The parameter names are

This parametrization needs the attitude of the satellite.

NameTypeAnnotation
inputfileAccelerometer
filename
estimateX
booleanalong
estimateY
booleancross
estimateZ
booleanradial
estimateCrossTalk
booleannon-orthognality of axes
estimateRotation
booleanmisalignment
temporal
parametrizationTemporal
perArc
boolean

GnssSolarRadiation

GNSS solar radiation pressure model. Paramters are estimated in $[nm/s^2=10^{-9}\,m/s^2]$.

The parameter names are

This parametrization needs the attitude of the satellite.

NameTypeAnnotation
estimateD0
booleanconstant term along D-axis (sat-sun vector)
estimateD2
boolean2-per-rev terms along D-axis
estimateD4
boolean4-per-rev terms along D-axis
estimateY0
booleanconstant term along Y-axis (solar panel axis)
estimateB0
booleanconstant term along B-axis (cross product D x Y)
estimateB1
boolean1-per-rev terms along B-axis
estimateB3
boolean3-per-rev terms along B-axis
perArc
boolean
eclipse
eclipse

ThermosphericDensity

Estimate the thermospheric density along the orbit using a satllite macro model. An optional thermospheric model can be used to compute temperature and wind. The temperature is used to estimate variable drag and lift coefficients, otherwise a constant drag coefficient is used. The density is estimated in $[kg/m^3]$.

The parameter names are *:density:<temporal>:<interval>.

This parametrization needs the macro model and the attitude of the satellite.

NameTypeAnnotation
thermosphere
thermospherefor wind and temperature
earthRotation
double[rad/s]
considerTemperature
booleancompute drag and lift, otherwise simple drag coefficient is used
considerWind
boolean
temporalDensity
parametrizationTemporalparameters along orbit
perArc
boolean

ModelScale

Estimate a scale factor for a given model. The parameter names are *:modelScale:<temporal>:<interval>.

NameTypeAnnotation
miscAccelerations
miscAccelerations
temporal
parametrizationTemporal
perArc
boolean