Serialized Form

Package org.orekit.rugged.errors

Class org.orekit.rugged.errors.RuggedException extends RuntimeException implements Serializable

serialVersionUID:

20140309L

Serialized Fields

parts

Object[] parts

Parts to insert in the format (no translation).

specifier

Localizable specifier

Format specifier (to be translated).

Class org.orekit.rugged.errors.RuggedExceptionWrapper extends RuntimeException implements Serializable

serialVersionUID:

20150224L

Serialized Fields

wrappedException

RuggedException wrappedException

Deprecated.

Underlying Orekit exception.

Class org.orekit.rugged.errors.RuggedInternalError extends RuntimeException implements Serializable

serialVersionUID:

20190305L

Serialized Fields

parts

String[] parts

Parts to insert in the format (no translation).

specifier

Localizable specifier

Format specifier (to be translated).

Package org.orekit.rugged.linesensor

Class org.orekit.rugged.linesensor.SensorPixel extends Object implements Serializable

serialVersionUID:

20140309L

Serialized Fields

lineNumber

double lineNumber

Line number.

pixelNumber

double pixelNumber

Pixel number.

Package org.orekit.rugged.utils

Class org.orekit.rugged.utils.ExtendedEllipsoid extends OneAxisEllipsoid implements Serializable

serialVersionUID:

20140312L

Serialized Fields

a2

double a2

Equatorial radius power 2.

b2

double b2

Polar radius power 2.

Class org.orekit.rugged.utils.NormalizedGeodeticPoint extends GeodeticPoint implements Serializable

serialVersionUID:

20141016L

Serialized Fields

normalizedLongitude

double normalizedLongitude

Normalized longitude.

Class org.orekit.rugged.utils.SpacecraftToObservedBody extends Object implements Serializable

serialVersionUID:

20140909L

Serialized Fields

bodyFrame

Frame bodyFrame

Body frame.

bodyToInertial

List<Transform> bodyToInertial

Transforms sample from observed body frame to inertial frame.

inertialFrame

Frame inertialFrame

Inertial frame.

inertialToBody

List<Transform> inertialToBody

Transforms sample from inertial frame to observed body frame.

maxDate

AbsoluteDate maxDate

End of search time span.

minDate

AbsoluteDate minDate

Start of search time span.

overshootTolerance

double overshootTolerance

Tolerance in seconds allowed for minDate and maxDate overshooting.

scToInertial

List<Transform> scToInertial

Transforms sample from spacecraft frame to inertial frame.

tStep

double tStep

Step to use for inertial frame to body frame transforms cache computations.