Download OpenAPI specification:Download
API for Flight Dynamics System
| date | string UTC date |
| frame required | string Enum: "EME2000" "ECI" "TEME" "GCRF" "GTOD" "ECF" "TNW" "QSW" Reference frame |
| id | string <uuid> |
| matrix required | Array of numbers[ items <double >[ items <double > ] ] |
| orbitType required | string Enum: "CARTESIAN" "KEPLERIAN" "EQUINOCTIAL" "CIRCULAR" |
{- "date": "string",
- "frame": "EME2000",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "matrix": [
- [
- 0.1
]
], - "orbitType": "CARTESIAN"
}{ }| date | string UTC date |
| diagonal required | Array of numbers <double> [ items <double > ] |
| frame required | string Enum: "EME2000" "ECI" "TEME" "GCRF" "GTOD" "ECF" "TNW" "QSW" Reference frame |
| id | string <uuid> |
| orbitType required | string Enum: "CARTESIAN" "KEPLERIAN" "EQUINOCTIAL" "CIRCULAR" |
{- "date": "string",
- "diagonal": [
- 0.1
], - "frame": "EME2000",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "orbitType": "CARTESIAN"
}{ }| altitudeStandardDeviation required | number <double> Units: [m] |
| dates required | Array of strings List of UTC dates |
| groundSpeedStandardDeviation required | number <double> Units: [m/s] |
| id | string <uuid> |
| latitudeStandardDeviation required | number <double> Units: [deg] |
| longitudeStandardDeviation required | number <double> Units: [deg] |
| measurements required | Array of numbers[ items <double >[ items <double > ] ] Array of double: latitude, longitude, norm of velocity in ECF frame, altitude, geoid separation. Units: [deg], [deg], [m/s], [m], [m] |
{- "altitudeStandardDeviation": 0.1,
- "dates": [
- "string"
], - "groundSpeedStandardDeviation": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "latitudeStandardDeviation": 0.1,
- "longitudeStandardDeviation": 0.1,
- "measurements": [
- [
- 0.1
]
]
}{ }| altitudeStandardDeviation required | number <double> Units: [m] |
| groundSpeedStandardDeviation required | number <double> Units: [m/s] |
| id | string <uuid> |
| latitudeStandardDeviation required | number <double> Units: [deg] |
| longitudeStandardDeviation required | number <double> Units: [deg] |
| nmeaSentences | Array of strings |
{- "altitudeStandardDeviation": 0.1,
- "groundSpeedStandardDeviation": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "latitudeStandardDeviation": 0.1,
- "longitudeStandardDeviation": 0.1,
- "nmeaSentences": [
- "string"
]
}{ }| dates required | Array of strings List of UTC dates |
| frame | string Enum: "EME2000" "ECI" "TEME" "GCRF" "GTOD" "ECF" "TNW" "QSW" Frame of definition of the position velocity vectors |
| id | string <uuid> |
| measurements required | Array of numbers[ items <double >[ items <double > ] ] List containing position and velocity vectors [x y z vx vy vz], Units: [m] [ms^-1] |
| positionStandardDeviation required | number <double> Units: [m] |
| velocityStandardDeviation required | number <double> Units: [ms^-1] |
{- "dates": [
- "string"
], - "frame": "EME2000",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "measurements": [
- [
- 0.1
]
], - "positionStandardDeviation": 0.1,
- "velocityStandardDeviation": 0.1
}{ }| azimuthStandardDeviation required | number <double> Units: [deg] |
| dates required | Array of strings List of UTC dates |
| elevationStandardDeviation required | number <double> Units: [deg] |
| groundStationId required | string <uuid> |
| id | string <uuid> |
| measurements required | Array of numbers[ items <double >[ items <double > ] ] Array of double: azimuth, elevation. Units: [deg], [deg] |
{- "azimuthStandardDeviation": 0.1,
- "dates": [
- "string"
], - "elevationStandardDeviation": 0.1,
- "groundStationId": "0e2bedfa-2c13-4217-8e1d-51aa401edc4b",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "measurements": [
- [
- 0.1
]
]
}{ }| azimuthStandardDeviation required | number <double> Units: [deg] |
| dates required | Array of strings List of UTC dates |
| elevationStandardDeviation required | number <double> Units: [deg] |
| groundStationId required | string <uuid> |
| id | string <uuid> |
| measurements required | Array of numbers[ items <double >[ items <double > ] ] Array of double: range, range rate, azimuth, elevation. Units: [m], [m/s], [deg], [deg] |
| rangeRateStandardDeviation required | number <double> Units: [m/s] |
| rangeStandardDeviation required | number <double> Units: [m] |
| twoWayMeasurement required | boolean |
{- "azimuthStandardDeviation": 0.1,
- "dates": [
- "string"
], - "elevationStandardDeviation": 0.1,
- "groundStationId": "0e2bedfa-2c13-4217-8e1d-51aa401edc4b",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "measurements": [
- [
- 0.1
]
], - "rangeRateStandardDeviation": 0.1,
- "rangeStandardDeviation": 0.1,
- "twoWayMeasurement": true
}{ }| id | string <uuid> |
| parameterStandardDeviation required | number <double> ( 0 .. 1 ] x in (0,1], Units: [-] |
| processNoiseStandardDeviation required | number <double> ( 0 .. 0.1 ] x in (0,0.1], Units: [-] |
{- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "parameterStandardDeviation": 0,
- "processNoiseStandardDeviation": 0
}{ }| id | string <uuid> |
| parameterStandardDeviation required | number <double> ( 0 .. 1 ] x in (0,1], Units: [-] |
| processNoiseStandardDeviation required | number <double> ( 0 .. 0.1 ] x in (0,0.1], Units: [-] |
{- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "parameterStandardDeviation": 0,
- "processNoiseStandardDeviation": 0
}{ }| id | string <uuid> |
| parameterStandardDeviation required | number <double> ( 0 .. 1 ] x in (0,1], Units: [-] |
| processNoiseStandardDeviation required | number <double> ( 0 .. 0.1 ] x in (0,0.1], Units: [-] |
{- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "parameterStandardDeviation": 0,
- "processNoiseStandardDeviation": 0
}{ }| ephemerisTypes required | Array of strings Items Enum: "CARTESIAN" "KEPLERIAN" "BATTERY" "QUATERNION" "THRUST" "EULER_ANGLES" List of requested ephemeris types |
| id | string <uuid> |
| step required | number <double> > 0 Units: [s] |
{- "ephemerisTypes": [
- "CARTESIAN"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "step": 0.1
}{- "ephemerisTypes": [
- "CARTESIAN"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "step": 0.1
}| alpha required | number <double> Defines the spread of the sigma points. Typical values from 1E-4 to 1E-1 |
| beta required | number <double> Incorporates knowledge about the distribution of the state vector. Beta = 2 is optimal for Gaussian distributions |
| id | string <uuid> |
| kappa required | number <double> Secondary scaling parameter. Usually set to 0 |
| noiseProviderType required | string Enum: "BASIC" "SNC" "DMC" "EDB_CD" Model for the state noise dynamics |
object (OutlierManagerSettingsDto) | |
| processNoiseMatrixId required | string <uuid> UUID of the covariance matrix for the state noise distribution |
{- "alpha": 0.1,
- "beta": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "kappa": 0.1,
- "noiseProviderType": "BASIC",
- "outlierManagerSettings": {
- "outlierManagerScale": 0.1,
- "outliersManagerWarmup": 0
}, - "processNoiseMatrixId": "609e5be9-1c17-490c-a238-867ec39256b1"
}{- "alpha": 0.1,
- "beta": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "kappa": 0.1,
- "noiseProviderType": "BASIC",
- "outlierManagerSettings": {
- "outlierManagerScale": 0.1,
- "outliersManagerWarmup": 0
}, - "processNoiseMatrixId": "609e5be9-1c17-490c-a238-867ec39256b1"
}| id required | string <uuid> |
{- "alpha": 0.1,
- "beta": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "kappa": 0.1,
- "noiseProviderType": "BASIC",
- "outlierManagerSettings": {
- "outlierManagerScale": 0.1,
- "outliersManagerWarmup": 0
}, - "processNoiseMatrixId": "609e5be9-1c17-490c-a238-867ec39256b1"
}[- {
- "alpha": 0.1,
- "beta": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "kappa": 0.1,
- "noiseProviderType": "BASIC",
- "outlierManagerSettings": {
- "outlierManagerScale": 0.1,
- "outliersManagerWarmup": 0
}, - "processNoiseMatrixId": "609e5be9-1c17-490c-a238-867ec39256b1"
}
]| id | string <uuid> |
| maximumPower | number <double> Units: [W] |
| satelliteFaces | Array of strings Items Enum: "PLUS_X" "MINUS_X" "PLUS_Y" "MINUS_Y" "PLUS_Z" "MINUS_Z" |
| solarArrayAxisInSatelliteFrame | Array of numbers <double> [ items <double > ] |
| solarArrayDefinitionType required | string Enum: "MAXIMUM_POWER" "SURFACE" "SURFACE_AND_POWER" |
| solarArrayEfficiency required | number <double> x in (0,1), Units: [-] |
| solarArrayNormalInSatelliteFrame required | Array of numbers <double> [ items <double > ] |
| solarArrayType required | string Enum: "SOLAR_ARRAY_TYPE_BODY" "SOLAR_ARRAY_TYPE_DEPLOYABLE_FIXED" "SOLAR_ARRAY_TYPE_DEPLOYABLE_ROTATING" "SOLAR_ARRAY_TYPE_NONE" |
| surface | number <double> Units: [m²] |
{- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "maximumPower": 0.1,
- "satelliteFaces": [
- "PLUS_X"
], - "solarArrayAxisInSatelliteFrame": [
- 0.1
], - "solarArrayDefinitionType": "MAXIMUM_POWER",
- "solarArrayEfficiency": 0.1,
- "solarArrayNormalInSatelliteFrame": [
- 0.1
], - "solarArrayType": "SOLAR_ARRAY_TYPE_BODY",
- "surface": 0.1
}{- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "maximumPower": 0.1,
- "satelliteFaces": [
- "PLUS_X"
], - "solarArrayAxisInSatelliteFrame": [
- 0.1
], - "solarArrayDefinitionType": "MAXIMUM_POWER",
- "solarArrayEfficiency": 0.1,
- "solarArrayNormalInSatelliteFrame": [
- 0.1
], - "solarArrayType": "SOLAR_ARRAY_TYPE_BODY",
- "surface": 0.1
}{- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "maximumPower": 0.1,
- "satelliteFaces": [
- "PLUS_X"
], - "solarArrayAxisInSatelliteFrame": [
- 0.1
], - "solarArrayDefinitionType": "MAXIMUM_POWER",
- "solarArrayEfficiency": 0.1,
- "solarArrayNormalInSatelliteFrame": [
- 0.1
], - "solarArrayType": "SOLAR_ARRAY_TYPE_BODY",
- "surface": 0.1
}[- {
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "maximumPower": 0.1,
- "satelliteFaces": [
- "PLUS_X"
], - "solarArrayAxisInSatelliteFrame": [
- 0.1
], - "solarArrayDefinitionType": "MAXIMUM_POWER",
- "solarArrayEfficiency": 0.1,
- "solarArrayNormalInSatelliteFrame": [
- 0.1
], - "solarArrayType": "SOLAR_ARRAY_TYPE_BODY",
- "surface": 0.1
}
]| deltaEccentricity required | number <double> Units: [-] |
| deltaInclination required | number <double> Units: [deg] |
| deltaSemiMajorAxis required | number <double> Units: [km] |
| initialOrbitalStateId required | string <uuid> |
| maximumDuration required | number <double> Units: [s] |
| quaternionStep required | number <double> Units: [s] |
| requiredOutputOrbitalStates required | string Enum: "ALL" "LAST" |
| strategyId required | string <uuid> |
{- "deltaEccentricity": 0.1,
- "deltaInclination": 0.1,
- "deltaSemiMajorAxis": 0.1,
- "initialOrbitalStateId": "d60137d3-8f02-459a-b1e1-02f8d1558b5d",
- "maximumDuration": 0.1,
- "quaternionStep": 0.1,
- "requiredOutputOrbitalStates": "ALL",
- "strategyId": "c855e259-15d8-4385-a60f-bdf8f7695ef7"
}{- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "log": {
- "computationDate": "2019-08-24T14:15:22Z",
- "computationStatus": "COMPUTATION_FAILURE",
- "errorMessages": [
- "string"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08"
}, - "report": {
- "averageThrustDuration": 0.1,
- "finalDutyCycle": 0.1,
- "numberOfPeriod": 0.1,
- "orbitalStates": [
- {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}
], - "simulationDuration": 0.1,
- "thrusterDutyCycle": 0.1,
- "totalBurnsDuration": 0.1,
- "totalConsumption": 0.1,
- "totalDeltaV": 0.1,
- "totalImpulse": 0.1,
- "totalNumberOfBurns": 0,
- "totalWarmupDutyCycle": 0.1
}, - "request": {
- "deltaEccentricity": 0.1,
- "deltaInclination": 0.1,
- "deltaSemiMajorAxis": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "initialOrbitalState": {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}, - "maximumDuration": 0.1,
- "quaternionStep": 0.1,
- "requiredOutputOrbitalStates": "ALL",
- "strategy": {
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "numberOfRestOrbits": 0,
- "numberOfShiftOrbits": 0,
- "numberOfThrustOrbits": 0,
- "orbitalDutyCycle": 0.1,
- "stopThrustAtEclipse": true,
- "thrustArcDefinition": "DUTY_CYCLE",
- "thrustArcDuration": 0.1,
- "thrustArcsNumber": "ONE",
- "thrustArcsPosition": "ASCENDING_AND_DESCENDING_NODES"
}
}, - "roadmap": { }
}| id required | string <uuid> |
{- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "log": {
- "computationDate": "2019-08-24T14:15:22Z",
- "computationStatus": "COMPUTATION_FAILURE",
- "errorMessages": [
- "string"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08"
}, - "report": {
- "averageThrustDuration": 0.1,
- "finalDutyCycle": 0.1,
- "numberOfPeriod": 0.1,
- "orbitalStates": [
- {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}
], - "simulationDuration": 0.1,
- "thrusterDutyCycle": 0.1,
- "totalBurnsDuration": 0.1,
- "totalConsumption": 0.1,
- "totalDeltaV": 0.1,
- "totalImpulse": 0.1,
- "totalNumberOfBurns": 0,
- "totalWarmupDutyCycle": 0.1
}, - "request": {
- "deltaEccentricity": 0.1,
- "deltaInclination": 0.1,
- "deltaSemiMajorAxis": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "initialOrbitalState": {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}, - "maximumDuration": 0.1,
- "quaternionStep": 0.1,
- "requiredOutputOrbitalStates": "ALL",
- "strategy": {
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "numberOfRestOrbits": 0,
- "numberOfShiftOrbits": 0,
- "numberOfThrustOrbits": 0,
- "orbitalDutyCycle": 0.1,
- "stopThrustAtEclipse": true,
- "thrustArcDefinition": "DUTY_CYCLE",
- "thrustArcDuration": 0.1,
- "thrustArcsNumber": "ONE",
- "thrustArcsPosition": "ASCENDING_AND_DESCENDING_NODES"
}
}, - "roadmap": { }
}{- "deltaEccentricity": 0.1,
- "deltaInclination": 0.1,
- "deltaSemiMajorAxis": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "initialOrbitalState": {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}, - "maximumDuration": 0.1,
- "quaternionStep": 0.1,
- "requiredOutputOrbitalStates": "ALL",
- "strategy": {
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "numberOfRestOrbits": 0,
- "numberOfShiftOrbits": 0,
- "numberOfThrustOrbits": 0,
- "orbitalDutyCycle": 0.1,
- "stopThrustAtEclipse": true,
- "thrustArcDefinition": "DUTY_CYCLE",
- "thrustArcDuration": 0.1,
- "thrustArcsNumber": "ONE",
- "thrustArcsPosition": "ASCENDING_AND_DESCENDING_NODES"
}
}| id required | string <uuid> |
[- {
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "log": {
- "computationDate": "2019-08-24T14:15:22Z",
- "computationStatus": "COMPUTATION_FAILURE",
- "errorMessages": [
- "string"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08"
}, - "report": {
- "averageThrustDuration": 0.1,
- "finalDutyCycle": 0.1,
- "numberOfPeriod": 0.1,
- "orbitalStates": [
- {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}
], - "simulationDuration": 0.1,
- "thrusterDutyCycle": 0.1,
- "totalBurnsDuration": 0.1,
- "totalConsumption": 0.1,
- "totalDeltaV": 0.1,
- "totalImpulse": 0.1,
- "totalNumberOfBurns": 0,
- "totalWarmupDutyCycle": 0.1
}, - "request": {
- "deltaEccentricity": 0.1,
- "deltaInclination": 0.1,
- "deltaSemiMajorAxis": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "initialOrbitalState": {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}, - "maximumDuration": 0.1,
- "quaternionStep": 0.1,
- "requiredOutputOrbitalStates": "ALL",
- "strategy": {
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "numberOfRestOrbits": 0,
- "numberOfShiftOrbits": 0,
- "numberOfThrustOrbits": 0,
- "orbitalDutyCycle": 0.1,
- "stopThrustAtEclipse": true,
- "thrustArcDefinition": "DUTY_CYCLE",
- "thrustArcDuration": 0.1,
- "thrustArcsNumber": "ONE",
- "thrustArcsPosition": "ASCENDING_AND_DESCENDING_NODES"
}
}, - "roadmap": { }
}
][- {
- "deltaEccentricity": 0.1,
- "deltaInclination": 0.1,
- "deltaSemiMajorAxis": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "initialOrbitalState": {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}, - "maximumDuration": 0.1,
- "quaternionStep": 0.1,
- "requiredOutputOrbitalStates": "ALL",
- "strategy": {
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "numberOfRestOrbits": 0,
- "numberOfShiftOrbits": 0,
- "numberOfThrustOrbits": 0,
- "orbitalDutyCycle": 0.1,
- "stopThrustAtEclipse": true,
- "thrustArcDefinition": "DUTY_CYCLE",
- "thrustArcDuration": 0.1,
- "thrustArcsNumber": "ONE",
- "thrustArcsPosition": "ASCENDING_AND_DESCENDING_NODES"
}
}
]| ephemerisRequestId | string <uuid> |
| eventsRequestIds | Array of strings <uuid> [ items <uuid > ] |
| extrapolateCovariance | boolean Should the covariance be propagated. Default is false |
| extrapolationDuration required | number <double> Units: [s] |
| initialOrbitalStateId required | string <uuid> |
| measurementsRequestId | string <uuid> |
| orbitDataMessageRequestId | string <uuid> |
| requiredOutputOrbitalStates | string Enum: "ALL" "LAST" Which orbital states should be included in the output |
| roadmapId | string <uuid> |
{- "ephemerisRequestId": "2556c3a9-f22f-458f-b4da-5c476fe859d9",
- "eventsRequestIds": [
- "497f6eca-6276-4993-bfeb-53cbbbba6f08"
], - "extrapolateCovariance": true,
- "extrapolationDuration": 0.1,
- "initialOrbitalStateId": "d60137d3-8f02-459a-b1e1-02f8d1558b5d",
- "measurementsRequestId": "745e562a-2600-4025-be5d-d430ff2dae4f",
- "orbitDataMessageRequestId": "7c9de407-bafe-41e3-b357-e37ccb8458fe",
- "requiredOutputOrbitalStates": "ALL",
- "roadmapId": "c17cc406-f776-4ae2-967c-6cc230b7f3bf"
}{- "computedEvents": [
- { }
], - "computedMeasurements": [
- { }
], - "ephemerides": [
- {
- "ephemerisType": "CARTESIAN",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "lines": [
- { }
]
}
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "log": {
- "computationDate": "2019-08-24T14:15:22Z",
- "computationStatus": "COMPUTATION_FAILURE",
- "errorMessages": [
- "string"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08"
}, - "orbitDataMessageOutput": "string",
- "orbitalStates": [
- {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}
], - "request": {
- "ephemerisRequest": {
- "ephemerisTypes": [
- "CARTESIAN"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "step": 0.1
}, - "eventsRequests": [
- { }
], - "extrapolateCovariance": true,
- "extrapolationDuration": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "initialOrbitalState": {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}, - "measurementsRequest": { },
- "orbitDataMessageRequest": { },
- "requiredOutputOrbitalStates": "ALL",
- "roadmap": { }
}
}| id required | string <uuid> |
{- "computedEvents": [
- { }
], - "computedMeasurements": [
- { }
], - "ephemerides": [
- {
- "ephemerisType": "CARTESIAN",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "lines": [
- { }
]
}
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "log": {
- "computationDate": "2019-08-24T14:15:22Z",
- "computationStatus": "COMPUTATION_FAILURE",
- "errorMessages": [
- "string"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08"
}, - "orbitDataMessageOutput": "string",
- "orbitalStates": [
- {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}
], - "request": {
- "ephemerisRequest": {
- "ephemerisTypes": [
- "CARTESIAN"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "step": 0.1
}, - "eventsRequests": [
- { }
], - "extrapolateCovariance": true,
- "extrapolationDuration": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "initialOrbitalState": {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}, - "measurementsRequest": { },
- "orbitDataMessageRequest": { },
- "requiredOutputOrbitalStates": "ALL",
- "roadmap": { }
}
}{- "ephemerisRequest": {
- "ephemerisTypes": [
- "CARTESIAN"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "step": 0.1
}, - "eventsRequests": [
- { }
], - "extrapolateCovariance": true,
- "extrapolationDuration": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "initialOrbitalState": {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}, - "measurementsRequest": { },
- "orbitDataMessageRequest": { },
- "requiredOutputOrbitalStates": "ALL",
- "roadmap": { }
}| id required | string <uuid> |
[- {
- "computedEvents": [
- { }
], - "computedMeasurements": [
- { }
], - "ephemerides": [
- {
- "ephemerisType": "CARTESIAN",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "lines": [
- { }
]
}
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "log": {
- "computationDate": "2019-08-24T14:15:22Z",
- "computationStatus": "COMPUTATION_FAILURE",
- "errorMessages": [
- "string"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08"
}, - "orbitDataMessageOutput": "string",
- "orbitalStates": [
- {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}
], - "request": {
- "ephemerisRequest": {
- "ephemerisTypes": [
- "CARTESIAN"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "step": 0.1
}, - "eventsRequests": [
- { }
], - "extrapolateCovariance": true,
- "extrapolationDuration": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "initialOrbitalState": {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}, - "measurementsRequest": { },
- "orbitDataMessageRequest": { },
- "requiredOutputOrbitalStates": "ALL",
- "roadmap": { }
}
}
][- {
- "ephemerisRequest": {
- "ephemerisTypes": [
- "CARTESIAN"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "step": 0.1
}, - "eventsRequests": [
- { }
], - "extrapolateCovariance": true,
- "extrapolationDuration": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "initialOrbitalState": {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}, - "measurementsRequest": { },
- "orbitDataMessageRequest": { },
- "requiredOutputOrbitalStates": "ALL",
- "roadmap": { }
}
]| date required | string UTC date |
| frame required | string Enum: "EME2000" "ECI" "TEME" "GCRF" "GTOD" "ECF" "TNW" "QSW" |
| id | string <uuid> |
| positionX required | number <double> Position X. Units: [km] |
| positionY required | number <double> Position Y. Units: [km] |
| positionZ required | number <double> Position Z. Units: [km] |
| velocityX required | number <double> Velocity X. Units: [km/s] |
| velocityY required | number <double> Velocity Y. Units: [km/s] |
| velocityZ required | number <double> Velocity Z. Units: [km/s] |
{- "date": "string",
- "frame": "EME2000",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "positionX": 0.1,
- "positionY": 0.1,
- "positionZ": 0.1,
- "velocityX": 0.1,
- "velocityY": 0.1,
- "velocityZ": 0.1
}{ }| argumentOfLatitude required | number <double> Units: [deg] |
| date required | string UTC date |
| eccentricityVectorX required | number <double> Eccentricity vector X. Units: [-] |
| eccentricityVectorY required | number <double> Eccentricity vector Y. Units: [-] |
| frame required | string Enum: "EME2000" "ECI" "TEME" "GCRF" "GTOD" "ECF" "TNW" "QSW" |
| id | string <uuid> |
| inclination required | number <double> Units: [deg] |
| meanOscType required | string Enum: "MEAN" "OSC" |
| positionAngleType required | string Enum: "TRUE" "MEAN" "ECCENTRIC" |
| raan required | number <double> Units: [deg] |
| semiMajorAxis required | number <double> Units: [km] |
{- "argumentOfLatitude": 0.1,
- "date": "string",
- "eccentricityVectorX": 0.1,
- "eccentricityVectorY": 0.1,
- "frame": "EME2000",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "inclination": 0.1,
- "meanOscType": "MEAN",
- "positionAngleType": "TRUE",
- "raan": 0.1,
- "semiMajorAxis": 0.1
}{ }| date required | string UTC date |
| eccentricityVectorX required | number <double> Eccentricity vector X. Units: [-] |
| eccentricityVectorY required | number <double> Eccentricity vector Y. Units: [-] |
| equinoctialLongitude required | number <double> Units: [deg] |
| frame required | string Enum: "EME2000" "ECI" "TEME" "GCRF" "GTOD" "ECF" "TNW" "QSW" |
| id | string <uuid> |
| inclinationVectorX required | number <double> Inclination vector X. Units: [-] |
| inclinationVectorY required | number <double> Inclination vector Y. Units: [-] |
| meanOscType required | string Enum: "MEAN" "OSC" |
| positionAngleType required | string Enum: "TRUE" "MEAN" "ECCENTRIC" |
| semiMajorAxis required | number <double> Units: [km] |
{- "date": "string",
- "eccentricityVectorX": 0.1,
- "eccentricityVectorY": 0.1,
- "equinoctialLongitude": 0.1,
- "frame": "EME2000",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "inclinationVectorX": 0.1,
- "inclinationVectorY": 0.1,
- "meanOscType": "MEAN",
- "positionAngleType": "TRUE",
- "semiMajorAxis": 0.1
}{ }| anomaly required | number <double> Units: [deg] |
| argumentOfPerigee required | number <double> Units: [deg] |
| date required | string UTC date |
| eccentricity required | number <double> Units: [-] |
| frame required | string Enum: "EME2000" "ECI" "TEME" "GCRF" "GTOD" "ECF" "TNW" "QSW" |
| id | string <uuid> |
| inclination required | number <double> Units: [deg] |
| meanOscType required | string Enum: "MEAN" "OSC" |
| positionAngleType required | string Enum: "TRUE" "MEAN" "ECCENTRIC" |
| raan required | number <double> Units: [deg] |
| semiMajorAxis required | number <double> Units: [km] |
{- "anomaly": 0.1,
- "argumentOfPerigee": 0.1,
- "date": "string",
- "eccentricity": 0.1,
- "frame": "EME2000",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "inclination": 0.1,
- "meanOscType": "MEAN",
- "positionAngleType": "TRUE",
- "raan": 0.1,
- "semiMajorAxis": 0.1
}{ }| covarianceMatrixId | string <uuid> |
| orbitId | string <uuid> Orbit ID (osculating or mean) is mandatory if no TLE is provided. |
| propagationContextId required | string <uuid> |
| spacecraftId required | string <uuid> |
object (TLE) |
{- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "orbitId": "1715fbdf-0ab7-4b83-a7d3-ef12b11aa213",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a",
- "tle": {
- "line1": "string",
- "line2": "string"
}
}{- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}{- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}[- {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}
]| altitudeStandardDeviation required | number <double> Expected altitude standard deviation. Units: [m] |
| generationStep required | integer <int32> Units: [s] |
| groundSpeedStandardDeviation required | number <double> Expected ground speed standard deviation. Units: [m/s] |
| id | string <uuid> |
| latitudeStandardDeviation required | number <double> Expected latitude standard deviation. Units: [deg] |
| longitudeStandardDeviation required | number <double> Expected longitude standard deviation. Units: [deg] |
{- "altitudeStandardDeviation": 0.1,
- "generationStep": 0,
- "groundSpeedStandardDeviation": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "latitudeStandardDeviation": 0.1,
- "longitudeStandardDeviation": 0.1
}{ }| frame required | string Enum: "EME2000" "ECI" "TEME" "GCRF" "GTOD" "ECF" "TNW" "QSW" |
| generationStep required | integer <int32> Units: [s] |
| id | string <uuid> |
| positionStandardDeviation required | number <double> Units: [m] |
| velocityStandardDeviation required | number <double> Units: [m/s] |
{- "frame": "EME2000",
- "generationStep": 0,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "positionStandardDeviation": 0.1,
- "velocityStandardDeviation": 0.1
}{ }| azimuthStandardDeviation required | number <double> Units: [deg] |
| elevationStandardDeviation required | number <double> Units: [deg] |
| generationStep required | integer <int32> Units: [s] |
| groundStationId required | string <uuid> The UUID of the observation station |
| id | string <uuid> |
{- "azimuthStandardDeviation": 0.1,
- "elevationStandardDeviation": 0.1,
- "generationStep": 0,
- "groundStationId": "0e2bedfa-2c13-4217-8e1d-51aa401edc4b",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08"
}{ }| azimuthStandardDeviation required | number <double> Units: [deg] |
| elevationStandardDeviation required | number <double> Units: [deg] |
| generationStep required | integer <int32> Units: [s] |
| groundStationId required | string <uuid> The UUID of the tracking station |
| id | string <uuid> |
| rangeRateStandardDeviation required | number <double> Units: [m/s] |
| rangeStandardDeviation required | number <double> Units: [m] |
| twoWayMeasurement required | boolean True for a two way signal |
{- "azimuthStandardDeviation": 0.1,
- "elevationStandardDeviation": 0.1,
- "generationStep": 0,
- "groundStationId": "0e2bedfa-2c13-4217-8e1d-51aa401edc4b",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "rangeRateStandardDeviation": 0.1,
- "rangeStandardDeviation": 0.1,
- "twoWayMeasurement": true
}{ }| dates required | Array of strings |
required | object (TLE) |
{- "dates": [
- "string"
], - "initialTle": {
- "line1": "string",
- "line2": "string"
}
}{- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "orbits": [
- { }
], - "tleExtrapolation": {
- "dates": [
- "string"
], - "initialTle": {
- "line1": "string",
- "line2": "string"
}
}
}{- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "orbits": [
- { }
], - "tleExtrapolation": {
- "dates": [
- "string"
], - "initialTle": {
- "line1": "string",
- "line2": "string"
}
}
}| id required | string <uuid> |
[- {
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "orbits": [
- { }
], - "tleExtrapolation": {
- "dates": [
- "string"
], - "initialTle": {
- "line1": "string",
- "line2": "string"
}
}
}
]| creator required | string |
| ephemeridesStep required | number <double> Units: [s] |
| frame required | string Enum: "EME2000" "ECI" "TEME" "GCRF" "GTOD" "ECF" "TNW" "QSW" The frame must be inertial |
| id | string <uuid> |
| objectId required | string |
| objectName required | string |
| writeAcceleration | boolean Include the accelerations in the output file |
| writeCovariance | boolean Include the covariance matrices in the output file |
{- "creator": "string",
- "ephemeridesStep": 0.1,
- "frame": "EME2000",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "objectId": "string",
- "objectName": "string",
- "writeAcceleration": true,
- "writeCovariance": true
}{ }| id required | string <uuid> |
{- "estimatedStates": [
- {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}
], - "firingAnalysisReport": {
- "failedAnalysesDates": [
- "2019-08-24T14:15:22Z"
], - "numberOfFailedAnalyses": 0,
- "numberOfPendingAnalyses": 0,
- "numberOfProcessedAnalyses": 0,
- "pendingAnalysesDates": [
- "2019-08-24T14:15:22Z"
], - "processedAnalyses": [
- {
- "argumentOfPerigeeDelta": 0.1,
- "date": "string",
- "eccentricityDelta": 0.1,
- "estimatedAcceleration": 0.1,
- "estimatedThrust": 0.1,
- "estimatedThrustTnwDirection": [
- 0.1
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "inclinationDelta": 0.1,
- "raanDelta": 0.1,
- "semiMajorAxisDelta": 0.1,
- "smoothedKeplerianElementsAfterFiring": {
- "argumentOfPerigee": 0.1,
- "argumentOfPerigeeStandardDeviation": 0.1,
- "eccentricity": 0.1,
- "eccentricityStandardDeviation": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "inclination": 0.1,
- "inclinationStandardDeviation": 0.1,
- "raan": 0.1,
- "raanStandardDeviation": 0.1,
- "semiMajorAxis": 0.1,
- "semiMajorAxisStandardDeviation": 0.1
}, - "smoothedKeplerianElementsBeforeFiring": {
- "argumentOfPerigee": 0.1,
- "argumentOfPerigeeStandardDeviation": 0.1,
- "eccentricity": 0.1,
- "eccentricityStandardDeviation": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "inclination": 0.1,
- "inclinationStandardDeviation": 0.1,
- "raan": 0.1,
- "raanStandardDeviation": 0.1,
- "semiMajorAxis": 0.1,
- "semiMajorAxisStandardDeviation": 0.1
}, - "status": "PROCESSED"
}
]
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "inDepthResults": {
- "covarianceMatrices": [
- { }
], - "estimatedDragCoefficients": [
- {
- "date": "string",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "value": 0.1
}
], - "estimatedReflectivityCoefficients": [
- {
- "date": "string",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "value": 0.1
}
], - "meanOrbits": [
- { }
], - "osculatingOrbits": [
- { }
]
}, - "log": {
- "computationDate": "2019-08-24T14:15:22Z",
- "computationStatus": "COMPUTATION_FAILURE",
- "errorMessages": [
- "string"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08"
}, - "report": {
- "numberOfRejectedMeasurements": 0,
- "numberOfUsedMeasurements": 0,
- "residualsStatistics": [
- {
- "field": "GPS_NMEA",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "mean": 0.1,
- "median": 0.1,
- "residuals": [
- {
- "date": "string",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "value": 0.1
}
], - "standardDeviation": 0.1
}
]
}, - "request": { },
- "status": "SUCCESS"
}| configurationId required | string <uuid> |
| estimatedResultsMinStep | number <double> Minimum step for the estimated results. Unit: s. |
| initialOrbitalStateId required | string <uuid> |
| parameterEstimationRequestIds | Array of strings <uuid> [ items <uuid > ] |
| roadmapId | string <uuid> |
| telemetryId required | string <uuid> |
{- "configurationId": "254ffdcc-3725-465c-b0a0-22afb2bec267",
- "estimatedResultsMinStep": 0.1,
- "initialOrbitalStateId": "d60137d3-8f02-459a-b1e1-02f8d1558b5d",
- "parameterEstimationRequestIds": [
- "497f6eca-6276-4993-bfeb-53cbbbba6f08"
], - "roadmapId": "c17cc406-f776-4ae2-967c-6cc230b7f3bf",
- "telemetryId": "d68cc54d-e0c9-4d44-be7d-1ee9a4219304"
}{- "estimatedStates": [
- {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}
], - "firingAnalysisReport": {
- "failedAnalysesDates": [
- "2019-08-24T14:15:22Z"
], - "numberOfFailedAnalyses": 0,
- "numberOfPendingAnalyses": 0,
- "numberOfProcessedAnalyses": 0,
- "pendingAnalysesDates": [
- "2019-08-24T14:15:22Z"
], - "processedAnalyses": [
- {
- "argumentOfPerigeeDelta": 0.1,
- "date": "string",
- "eccentricityDelta": 0.1,
- "estimatedAcceleration": 0.1,
- "estimatedThrust": 0.1,
- "estimatedThrustTnwDirection": [
- 0.1
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "inclinationDelta": 0.1,
- "raanDelta": 0.1,
- "semiMajorAxisDelta": 0.1,
- "smoothedKeplerianElementsAfterFiring": {
- "argumentOfPerigee": 0.1,
- "argumentOfPerigeeStandardDeviation": 0.1,
- "eccentricity": 0.1,
- "eccentricityStandardDeviation": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "inclination": 0.1,
- "inclinationStandardDeviation": 0.1,
- "raan": 0.1,
- "raanStandardDeviation": 0.1,
- "semiMajorAxis": 0.1,
- "semiMajorAxisStandardDeviation": 0.1
}, - "smoothedKeplerianElementsBeforeFiring": {
- "argumentOfPerigee": 0.1,
- "argumentOfPerigeeStandardDeviation": 0.1,
- "eccentricity": 0.1,
- "eccentricityStandardDeviation": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "inclination": 0.1,
- "inclinationStandardDeviation": 0.1,
- "raan": 0.1,
- "raanStandardDeviation": 0.1,
- "semiMajorAxis": 0.1,
- "semiMajorAxisStandardDeviation": 0.1
}, - "status": "PROCESSED"
}
]
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "inDepthResults": {
- "covarianceMatrices": [
- { }
], - "estimatedDragCoefficients": [
- {
- "date": "string",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "value": 0.1
}
], - "estimatedReflectivityCoefficients": [
- {
- "date": "string",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "value": 0.1
}
], - "meanOrbits": [
- { }
], - "osculatingOrbits": [
- { }
]
}, - "log": {
- "computationDate": "2019-08-24T14:15:22Z",
- "computationStatus": "COMPUTATION_FAILURE",
- "errorMessages": [
- "string"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08"
}, - "report": {
- "numberOfRejectedMeasurements": 0,
- "numberOfUsedMeasurements": 0,
- "residualsStatistics": [
- {
- "field": "GPS_NMEA",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "mean": 0.1,
- "median": 0.1,
- "residuals": [
- {
- "date": "string",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "value": 0.1
}
], - "standardDeviation": 0.1
}
]
}, - "request": { },
- "status": "SUCCESS"
}| id required | string <uuid> |
[- {
- "estimatedStates": [
- {
- "covarianceMatrixId": "5b5ec652-36e4-4616-a0d9-707fed44d34c",
- "creationDate": "string",
- "fittedTle": {
- "line1": "string",
- "line2": "string"
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "meanOrbitId": "dac2598d-25aa-4954-afea-11d2e99e0b13",
- "osculatingOrbitId": "82197dae-a047-454b-8bad-04fc81ad59d4",
- "propagationContextId": "13f9c5e0-1189-48c8-9910-4eb211e07b0a",
- "source": "ORBIT_DETERMINATION",
- "spacecraftId": "10d939b7-63d0-4441-a1c9-dc380aafe23a"
}
], - "firingAnalysisReport": {
- "failedAnalysesDates": [
- "2019-08-24T14:15:22Z"
], - "numberOfFailedAnalyses": 0,
- "numberOfPendingAnalyses": 0,
- "numberOfProcessedAnalyses": 0,
- "pendingAnalysesDates": [
- "2019-08-24T14:15:22Z"
], - "processedAnalyses": [
- {
- "argumentOfPerigeeDelta": 0.1,
- "date": "string",
- "eccentricityDelta": 0.1,
- "estimatedAcceleration": 0.1,
- "estimatedThrust": 0.1,
- "estimatedThrustTnwDirection": [
- 0.1
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "inclinationDelta": 0.1,
- "raanDelta": 0.1,
- "semiMajorAxisDelta": 0.1,
- "smoothedKeplerianElementsAfterFiring": {
- "argumentOfPerigee": 0.1,
- "argumentOfPerigeeStandardDeviation": 0.1,
- "eccentricity": 0.1,
- "eccentricityStandardDeviation": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "inclination": 0.1,
- "inclinationStandardDeviation": 0.1,
- "raan": 0.1,
- "raanStandardDeviation": 0.1,
- "semiMajorAxis": 0.1,
- "semiMajorAxisStandardDeviation": 0.1
}, - "smoothedKeplerianElementsBeforeFiring": {
- "argumentOfPerigee": 0.1,
- "argumentOfPerigeeStandardDeviation": 0.1,
- "eccentricity": 0.1,
- "eccentricityStandardDeviation": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "inclination": 0.1,
- "inclinationStandardDeviation": 0.1,
- "raan": 0.1,
- "raanStandardDeviation": 0.1,
- "semiMajorAxis": 0.1,
- "semiMajorAxisStandardDeviation": 0.1
}, - "status": "PROCESSED"
}
]
}, - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "inDepthResults": {
- "covarianceMatrices": [
- { }
], - "estimatedDragCoefficients": [
- {
- "date": "string",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "value": 0.1
}
], - "estimatedReflectivityCoefficients": [
- {
- "date": "string",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "value": 0.1
}
], - "meanOrbits": [
- { }
], - "osculatingOrbits": [
- { }
]
}, - "log": {
- "computationDate": "2019-08-24T14:15:22Z",
- "computationStatus": "COMPUTATION_FAILURE",
- "errorMessages": [
- "string"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08"
}, - "report": {
- "numberOfRejectedMeasurements": 0,
- "numberOfUsedMeasurements": 0,
- "residualsStatistics": [
- {
- "field": "GPS_NMEA",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "mean": 0.1,
- "median": 0.1,
- "residuals": [
- {
- "date": "string",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "value": 0.1
}
], - "standardDeviation": 0.1
}
]
}, - "request": { },
- "status": "SUCCESS"
}
]| depthOfDischarge required | number <double> [ 0 .. 1 ] x in (0,1), Units: [-] |
| id | string <uuid> |
| initialCharge required | number <double> [ 0 .. 1 ] x in (0,1], Units: [-] |
| minimumChargeForFiring required | number <double> [ 0 .. 1 ] x in (0,1), Units: [-] |
| nominalCapacity required | number <double> >= 0 Units: [Wh] |
{- "depthOfDischarge": 1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "initialCharge": 1,
- "minimumChargeForFiring": 1,
- "nominalCapacity": 0.1
}{- "depthOfDischarge": 1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "initialCharge": 1,
- "minimumChargeForFiring": 1,
- "nominalCapacity": 0.1
}[- {
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "numberOfRestOrbits": 0,
- "numberOfShiftOrbits": 0,
- "numberOfThrustOrbits": 0,
- "orbitalDutyCycle": 0.1,
- "stopThrustAtEclipse": true,
- "thrustArcDefinition": "DUTY_CYCLE",
- "thrustArcDuration": 0.1,
- "thrustArcsNumber": "ONE",
- "thrustArcsPosition": "ASCENDING_AND_DESCENDING_NODES"
}
]| id | string <uuid> |
| numberOfRestOrbits required | integer <int32> Units: [-] |
| numberOfShiftOrbits required | integer <int32> Units: [-] |
| numberOfThrustOrbits required | integer <int32> Units: [-] |
| orbitalDutyCycle | number <double> Units: [%] |
| stopThrustAtEclipse required | boolean |
| thrustArcDefinition required | string Enum: "DUTY_CYCLE" "THRUST_DURATION" |
| thrustArcDuration | number <double> Units: [s] |
| thrustArcsNumber required | string Enum: "ONE" "TWO" |
| thrustArcsPosition required | string Enum: "ASCENDING_AND_DESCENDING_NODES" "ASCENDING_NODE" "CUSTOM" "DESCENDING_NODE" "APOGEE_AND_PERIGEE" "APOGEE" "PERIGEE" "ASCENDING_AND_DESCENDING_ANTINODES" "ASCENDING_ANTINODE" "DESCENDING_ANTINODE" "MEAN_LONGITUDE" |
{- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "numberOfRestOrbits": 0,
- "numberOfShiftOrbits": 0,
- "numberOfThrustOrbits": 0,
- "orbitalDutyCycle": 0.1,
- "stopThrustAtEclipse": true,
- "thrustArcDefinition": "DUTY_CYCLE",
- "thrustArcDuration": 0.1,
- "thrustArcsNumber": "ONE",
- "thrustArcsPosition": "ASCENDING_AND_DESCENDING_NODES"
}{- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "numberOfRestOrbits": 0,
- "numberOfShiftOrbits": 0,
- "numberOfThrustOrbits": 0,
- "orbitalDutyCycle": 0.1,
- "stopThrustAtEclipse": true,
- "thrustArcDefinition": "DUTY_CYCLE",
- "thrustArcDuration": 0.1,
- "thrustArcsNumber": "ONE",
- "thrustArcsPosition": "ASCENDING_AND_DESCENDING_NODES"
}| id required | string <uuid> |
{- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "numberOfRestOrbits": 0,
- "numberOfShiftOrbits": 0,
- "numberOfThrustOrbits": 0,
- "orbitalDutyCycle": 0.1,
- "stopThrustAtEclipse": true,
- "thrustArcDefinition": "DUTY_CYCLE",
- "thrustArcDuration": 0.1,
- "thrustArcsNumber": "ONE",
- "thrustArcsPosition": "ASCENDING_AND_DESCENDING_NODES"
}| batteryId required | string <uuid> |
| dragCoefficient required | number <double> Units: [-] |
| id | string <uuid> |
| maxAngularAcceleration required | number <double> Units: [deg/s²] |
| maxAngularVelocity required | number <double> Units: [deg/s] |
| platformMass required | number <double> |
| reflectionCoefficient | number <double> Units: [-] |
| solarArrayId required | string <uuid> |
| spacecraftLengthX required | number <double> Units: [m] |
| spacecraftLengthY required | number <double> Units: [m] |
| spacecraftLengthZ required | number <double> Units: [m] |
| thrusterId required | string <uuid> |
{- "batteryId": "c2b3dd8f-c3ea-4036-9ad2-c21f056c3506",
- "dragCoefficient": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "maxAngularAcceleration": 0.1,
- "maxAngularVelocity": 0.1,
- "platformMass": 0.1,
- "reflectionCoefficient": 0.1,
- "solarArrayId": "77b1aa4c-e672-446e-9a7d-e261d263336f",
- "spacecraftLengthX": 0.1,
- "spacecraftLengthY": 0.1,
- "spacecraftLengthZ": 0.1,
- "thrusterId": "f558f6c8-2eb4-4ff1-8f14-b1e59e289093"
}{ }| dragCoefficient required | number <double> Units: [-] |
| id | string <uuid> |
| platformMass required | number <double> Units: [kg] |
| reflectionCoefficient | number <double> Units: [-] |
| sphericalCrossSection required | number <double> Units: [m²] |
{- "dragCoefficient": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "platformMass": 0.1,
- "reflectionCoefficient": 0.1,
- "sphericalCrossSection": 0.1
}{ }| id | string <uuid> |
| impulse required | number <double> Units: [Ns] |
| maximumThrustDuration required | number <double> Units: [s] |
| propellantMass required | number <double> Units: [kg] |
| thrust required | number <double> Units: [N] |
| thrusterAxisInSatelliteFrame required | Array of numbers <double> [ items <double > ] |
| thrusterIsp required | number <double> Units: [s] |
| thrusterTotalMass required | number <double> Wet mass. Units: [kg] |
| warmUpDuration required | number <double> Units: [s] |
{- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "impulse": 0.1,
- "maximumThrustDuration": 0.1,
- "propellantMass": 0.1,
- "thrust": 0.1,
- "thrusterAxisInSatelliteFrame": [
- 0.1
], - "thrusterIsp": 0.1,
- "thrusterTotalMass": 0.1,
- "warmUpDuration": 0.1
}{ }| id | string <uuid> |
| impulse required | number <double> Units: [Ns] |
| maximumThrustDuration required | number <double> Units: [s] |
| propellantMass required | number <double> Units: [kg] |
| standByPower required | number <double> Units: [W] |
| thrust required | number <double> Units: [N] |
| thrusterAxisInSatelliteFrame required | Array of numbers <double> [ items <double > ] |
| thrusterIsp required | number <double> Units: [s] |
| thrusterPower required | number <double> Units: [W] |
| thrusterTotalMass required | number <double> Wet mass. Units: [kg] |
| warmUpDuration required | number <double> Units: [s] |
| warmUpPower required | number <double> Units: [W] |
{- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "impulse": 0.1,
- "maximumThrustDuration": 0.1,
- "propellantMass": 0.1,
- "standByPower": 0.1,
- "thrust": 0.1,
- "thrusterAxisInSatelliteFrame": [
- 0.1
], - "thrusterIsp": 0.1,
- "thrusterPower": 0.1,
- "thrusterTotalMass": 0.1,
- "warmUpDuration": 0.1,
- "warmUpPower": 0.1
}{ }| finalDate required | string UTC date |
| id | string <uuid> |
| initialDate required | string UTC date |
| roadmapActionIDs required | Array of strings <uuid> [ items <uuid > ] The UUIDs of the roadmap actions (firing, attitude or quaternion) to be executed |
{- "finalDate": "string",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "initialDate": "string",
- "roadmapActionIDs": [
- "497f6eca-6276-4993-bfeb-53cbbbba6f08"
]
}{ }| eventsType required | Array of strings Items Enum: "NODE" "ECLIPSE" "ORBITAL_6AMPM" "ORBITAL_NOON_MIDNIGHT" "APSIDE" |
| id | string <uuid> |
| startDate | string UTC date |
{- "eventsType": [
- "NODE"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "startDate": "string"
}{ }| ephemeridesStep required | number <double> |
| eventsType required | Array of strings Items Value: "SUN_IN_FOV" |
| id | string <uuid> |
| sensorAxisInSpacecraftFrame required | Array of numbers <double> [ items <double > ] |
| sensorFieldOfViewHalfAngle required | number <double> The half angle defining the conical field of view. Units [deg] |
| startDate | string UTC date |
{- "ephemeridesStep": 0.1,
- "eventsType": [
- "SUN_IN_FOV"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "sensorAxisInSpacecraftFrame": [
- 0.1
], - "sensorFieldOfViewHalfAngle": 0.1,
- "startDate": "string"
}{ }| groundStationIDs required | Array of strings <uuid> [ items <uuid > ] The station's UUID |
| id | string <uuid> |
| startDate | string UTC date |
{- "groundStationIDs": [
- "497f6eca-6276-4993-bfeb-53cbbbba6f08"
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "startDate": "string"
}{ }| altitude required | number <double> Units: [km] |
| elevationMask | Array of numbers[ items <double >[ items <double > ] ] Units: Double[deg][deg] |
| id | string <uuid> |
| latitude required | number <double> Units: [deg] |
| longitude required | number <double> Units: [deg] |
| minElevation | number <double> Units: [deg] |
| name required | string |
{- "altitude": 0.1,
- "elevationMask": [
- [
- 0.1
]
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "latitude": 0.1,
- "longitude": 0.1,
- "minElevation": 0.1,
- "name": "string"
}{- "altitude": 0.1,
- "elevationMask": [
- [
- 0.1
]
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "latitude": 0.1,
- "longitude": 0.1,
- "minElevation": 0.1,
- "name": "string"
}{- "altitude": 0.1,
- "elevationMask": [
- [
- 0.1
]
], - "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "latitude": 0.1,
- "longitude": 0.1,
- "minElevation": 0.1,
- "name": "string"
}| atmosphereType | string Enum: "HARRIS_PRIESTER" "NRL_MSISE00" Required if perturbations include DRAG |
| earthPotentialDeg | integer <int32> >= 2 Required if perturbations include EARTH_POTENTIAL. Value must be earthPotentialDeg > 2. Units: [-] |
| earthPotentialOrd | integer <int32> Required if perturbations include EARTH_POTENTIAL. Value must be 0 <= earthPotentialOrd <= earthPotentialDeg. Units: [-] |
| id | string <uuid> |
| integratorMaxStep | number <double> [ 0.001 .. 86400 ] Default: 100 Units: [s]. Default 100 s. Must be integratorMaxStep > integratorMinStep. |
| integratorMinStep | number <double> [ 0.001 .. 86400 ] Default: 0.01 Units: [s]. Default 0.01 s. Must be integratorMinStep > 0.001 s. |
| integratorType | string Enum: "DORMAND_PRINCE_853" "DORMAND_PRINCE_54" "ADAMS_MOULTON" "RUNGE_KUTTA" |
| perturbations | Array of strings unique Items Enum: "EARTH_POTENTIAL" "SRP" "THIRD_BODY" "DRAG" "CONSTANT_THRUST" "IMPULSIVE_THRUST" Default to DORMAND_PRINCE_853. |
| solarFlux | number <double> Required if perturbations include DRAG. Units: [sfu] |
{- "atmosphereType": "HARRIS_PRIESTER",
- "earthPotentialDeg": 2,
- "earthPotentialOrd": 0,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "integratorMaxStep": 100,
- "integratorMinStep": 0.01,
- "integratorType": "DORMAND_PRINCE_853",
- "perturbations": [
- "EARTH_POTENTIAL"
], - "solarFlux": 0.1
}{- "atmosphereType": "HARRIS_PRIESTER",
- "earthPotentialDeg": 2,
- "earthPotentialOrd": 0,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "integratorMaxStep": 100,
- "integratorMinStep": 0.01,
- "integratorType": "DORMAND_PRINCE_853",
- "perturbations": [
- "EARTH_POTENTIAL"
], - "solarFlux": 0.1
}{- "atmosphereType": "HARRIS_PRIESTER",
- "earthPotentialDeg": 2,
- "earthPotentialOrd": 0,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "integratorMaxStep": 100,
- "integratorMinStep": 0.01,
- "integratorType": "DORMAND_PRINCE_853",
- "perturbations": [
- "EARTH_POTENTIAL"
], - "solarFlux": 0.1
}[- {
- "atmosphereType": "HARRIS_PRIESTER",
- "earthPotentialDeg": 2,
- "earthPotentialOrd": 0,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "integratorMaxStep": 100,
- "integratorMinStep": 0.01,
- "integratorType": "DORMAND_PRINCE_853",
- "perturbations": [
- "EARTH_POTENTIAL"
], - "solarFlux": 0.1
}
]| attitudeMode required | string Enum: "PROGRADE" "RETROGRADE" "NORMAL" "ANTI_NORMAL" "RADIAL" "ANTI_RADIAL" "QUATERNION" "NONE" "SUN_POINTING" "TELECOM" "PAYLOAD" "TRANSITIONAL" "LOF_ALIGNED_LVLH_CCSDS" "RETROGRADE_NADIR" Attitude list, can contains quaternions |
| id | string <uuid> |
Array of objects (QuaternionActionDto) List of quaternions related to the current attitude. Required if attitudeMode is QUATERNION | |
| transitionDate required | string UTC date |
{- "attitudeMode": "PROGRADE",
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "quaternions": [
- {
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "q0": 1,
- "q1": 0.1,
- "q2": 0.1,
- "q3": 0.1,
- "transitionDate": "string"
}
], - "transitionDate": "string"
}{ }| firingAttitude required | string Enum: "PROGRADE" "RETROGRADE" "NORMAL" "ANTI_NORMAL" "RADIAL" "ANTI_RADIAL" "QUATERNION" "NONE" "SUN_POINTING" "TELECOM" "PAYLOAD" "TRANSITIONAL" "LOF_ALIGNED_LVLH_CCSDS" "RETROGRADE_NADIR" |
| firingDuration required | number <double> Units: [s] |
| id | string <uuid> |
| postFiringAttitude required | string Enum: "PROGRADE" "RETROGRADE" "NORMAL" "ANTI_NORMAL" "RADIAL" "ANTI_RADIAL" "QUATERNION" "NONE" "SUN_POINTING" "TELECOM" "PAYLOAD" "TRANSITIONAL" "LOF_ALIGNED_LVLH_CCSDS" "RETROGRADE_NADIR" |
| startFiring required | string UTC date |
| warmUpAttitude | string Enum: "PROGRADE" "RETROGRADE" "NORMAL" "ANTI_NORMAL" "RADIAL" "ANTI_RADIAL" "QUATERNION" "NONE" "SUN_POINTING" "TELECOM" "PAYLOAD" "TRANSITIONAL" "LOF_ALIGNED_LVLH_CCSDS" "RETROGRADE_NADIR" |
| warmUpDuration required | number <double> Units: [s] |
{- "firingAttitude": "PROGRADE",
- "firingDuration": 0.1,
- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "postFiringAttitude": "PROGRADE",
- "startFiring": "string",
- "warmUpAttitude": "PROGRADE",
- "warmUpDuration": 0.1
}{ }| id | string <uuid> |
| q0 required | number <double> Default: 1 Scalar component. Units: [-] |
| q1 required | number <double> Vector part of the quaternion. First component. Units: [-] |
| q2 required | number <double> Vector part of the quaternion. Second component. Units: [-] |
| q3 required | number <double> Vector part of the quaternion. Third component. Units: [-] |
| transitionDate required | string UTC date |
{- "id": "497f6eca-6276-4993-bfeb-53cbbbba6f08",
- "q0": 1,
- "q1": 0.1,
- "q2": 0.1,
- "q3": 0.1,
- "transitionDate": "string"
}{ }