public interface DragSensitive
DragForce
Modifier and Type | Field and Description |
---|---|
static String |
DRAG_COEFFICIENT
Parameter name for drag coefficient enabling jacobian processing.
|
Modifier and Type | Method and Description |
---|---|
FieldVector3D<DerivativeStructure> |
dragAcceleration(AbsoluteDate date,
Frame frame,
FieldVector3D<DerivativeStructure> position,
FieldRotation<DerivativeStructure> rotation,
DerivativeStructure mass,
DerivativeStructure density,
FieldVector3D<DerivativeStructure> relativeVelocity)
Compute the acceleration due to drag, with state derivatives.
|
Vector3D |
dragAcceleration(AbsoluteDate date,
Frame frame,
Vector3D position,
Rotation rotation,
double mass,
double density,
Vector3D relativeVelocity)
Compute the acceleration due to drag.
|
FieldVector3D<DerivativeStructure> |
dragAcceleration(AbsoluteDate date,
Frame frame,
Vector3D position,
Rotation rotation,
double mass,
double density,
Vector3D relativeVelocity,
String paramName)
Compute acceleration due to drag, with parameters derivatives.
|
default double |
getDragCoefficient()
Deprecated.
as of 8.0, replaced with
getDragParametersDrivers() |
ParameterDriver[] |
getDragParametersDrivers()
Get the drivers for supported parameters.
|
default List<String> |
getDragParametersNames()
Deprecated.
as of 8.0, replaced with
getDragParametersDrivers() |
default void |
setDragCoefficient(double value)
Deprecated.
as of 8.0, replaced with
getDragParametersDrivers() |
static final String DRAG_COEFFICIENT
ParameterDriver[] getDragParametersDrivers()
Vector3D dragAcceleration(AbsoluteDate date, Frame frame, Vector3D position, Rotation rotation, double mass, double density, Vector3D relativeVelocity) throws OrekitException
The computation includes all spacecraft specific characteristics like shape, area and coefficients.
date
- current dateframe
- inertial reference frame for state (both orbit and attitude)position
- position of spacecraft in reference framerotation
- orientation (attitude) of the spacecraft with respect to reference framemass
- current massdensity
- atmospheric density at spacecraft positionrelativeVelocity
- relative velocity of atmosphere with respect to spacecraft,
in the same inertial frame as spacecraft orbit (m/s)OrekitException
- if acceleration cannot be computedFieldVector3D<DerivativeStructure> dragAcceleration(AbsoluteDate date, Frame frame, FieldVector3D<DerivativeStructure> position, FieldRotation<DerivativeStructure> rotation, DerivativeStructure mass, DerivativeStructure density, FieldVector3D<DerivativeStructure> relativeVelocity) throws OrekitException
The computation includes all spacecraft specific characteristics like shape, area and coefficients.
date
- current dateframe
- inertial reference frame for state (both orbit and attitude)position
- position of spacecraft in reference framerotation
- orientation (attitude) of the spacecraft with respect to reference framemass
- spacecraft massdensity
- atmospheric density at spacecraft positionrelativeVelocity
- relative velocity of atmosphere with respect to spacecraft,
in the same inertial frame as spacecraft orbit (m/s)OrekitException
- if acceleration cannot be computedFieldVector3D<DerivativeStructure> dragAcceleration(AbsoluteDate date, Frame frame, Vector3D position, Rotation rotation, double mass, double density, Vector3D relativeVelocity, String paramName) throws OrekitException
date
- current dateframe
- inertial reference frame for state (both orbit and attitude)position
- position of spacecraft in reference framerotation
- orientation (attitude) of the spacecraft with respect to reference framemass
- current massdensity
- atmospheric density at spacecraft positionrelativeVelocity
- relative velocity of atmosphere with respect to spacecraft,
in the same inertial frame as spacecraft orbit (m/s)paramName
- name of the parameter with respect to which derivatives are requiredOrekitException
- if derivatives cannot be computed@Deprecated default List<String> getDragParametersNames()
getDragParametersDrivers()
@Deprecated default void setDragCoefficient(double value) throws OrekitException
getDragParametersDrivers()
value
- absorption coefficientOrekitException
- if parameter cannot be set@Deprecated default double getDragCoefficient() throws OrekitException
getDragParametersDrivers()
OrekitException
- if parameter cannot be setCopyright © 2002-2016 CS Systèmes d'information. All rights reserved.