diff --git a/orekit_jpype/jars/orekit-12.1.1.jar b/orekit_jpype/jars/orekit-12.1.2.jar
similarity index 90%
rename from orekit_jpype/jars/orekit-12.1.1.jar
rename to orekit_jpype/jars/orekit-12.1.2.jar
index 3bbe1578e8af4c0efa3e9aa4bcaace8f07067673..19bed4da8c6a31d494c344b731c351aa1dc6e24c 100644
Binary files a/orekit_jpype/jars/orekit-12.1.1.jar and b/orekit_jpype/jars/orekit-12.1.2.jar differ
diff --git a/org-stubs/orekit/forces/maneuvers/trigger/__init__.pyi b/org-stubs/orekit/forces/maneuvers/trigger/__init__.pyi
index 832a2a9a3c3d89e9c549df42397c876faabbbd8e..c9458dba04f511f3d96013262706cbae62a5f314 100644
--- a/org-stubs/orekit/forces/maneuvers/trigger/__init__.pyi
+++ b/org-stubs/orekit/forces/maneuvers/trigger/__init__.pyi
@@ -344,6 +344,50 @@ class IntervalEventTrigger(AbstractManeuverTriggers, typing.Generic[_IntervalEve
firing interval detector
+ """
+ ...
+ _init_0__D = typing.TypeVar('_init_0__D', bound=org.hipparchus.CalculusFieldElement) # <D>
+ @typing.overload
+ def init(self, fieldSpacecraftState: org.orekit.propagation.FieldSpacecraftState[_init_0__D], fieldAbsoluteDate: org.orekit.time.FieldAbsoluteDate[_init_0__D]) -> None:
+ """
+ Initialization method called at propagation start.
+
+ The default implementation does nothing.
+
+ Specified by:
+ :meth:`~org.orekit.forces.maneuvers.trigger.ManeuverTriggers.init` in
+ interface :class:`~org.orekit.forces.maneuvers.trigger.ManeuverTriggers`
+
+ Overrides:
+ :meth:`~org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers.init` in
+ class :class:`~org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers`
+
+ Parameters:
+ initialState (:class:`~org.orekit.propagation.FieldSpacecraftState`<D> initialState): initial spacecraft state (at the start of propagation).
+ target (:class:`~org.orekit.time.FieldAbsoluteDate`<D> target): date of propagation. Not equal to :code:`initialState.getDate()`.
+
+
+ """
+ ...
+ @typing.overload
+ def init(self, spacecraftState: org.orekit.propagation.SpacecraftState, absoluteDate: org.orekit.time.AbsoluteDate) -> None:
+ """
+ Initialization method called at propagation start.
+
+ The default implementation does nothing.
+
+ Specified by:
+ :meth:`~org.orekit.forces.maneuvers.trigger.ManeuverTriggers.init` in
+ interface :class:`~org.orekit.forces.maneuvers.trigger.ManeuverTriggers`
+
+ Overrides:
+ :meth:`~org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers.init` in
+ class :class:`~org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers`
+
+ Parameters:
+ initialState (:class:`~org.orekit.propagation.SpacecraftState`): initial spacecraft state (at the start of propagation).
+ target (:class:`~org.orekit.time.AbsoluteDate`): date of propagation. Not equal to :code:`initialState.getDate()`.
+
"""
...
diff --git a/org-stubs/orekit/models/earth/troposphere/__init__.pyi b/org-stubs/orekit/models/earth/troposphere/__init__.pyi
index a859ac0b847093e3efdf901624c2caed7a304571..6461dba061152101ab3c10d74c856e411c5c4cd3 100644
--- a/org-stubs/orekit/models/earth/troposphere/__init__.pyi
+++ b/org-stubs/orekit/models/earth/troposphere/__init__.pyi
@@ -2102,7 +2102,23 @@ class ModifiedSaastamoinenModel(TroposphericModel, DiscreteTroposphericModel):
"""
...
@staticmethod
- def getStandardModel() -> 'ModifiedSaastamoinenModel': ...
+ def getStandardModel() -> 'ModifiedSaastamoinenModel':
+ """
+ Create a new Saastamoinen model using a standard atmosphere model.
+
+ - altitude: 0m
+ - temperature: 18 degree Celsius
+ - pressure: 1013.25 mbar
+ - humidity: 50%
+ - @link :class:`~org.orekit.models.earth.weather.water.Wang1988` model to compute water vapor pressure
+
+
+ Returns:
+ a Saastamoinen model with standard environmental values
+
+
+ """
+ ...
_pathDelay_1__T = typing.TypeVar('_pathDelay_1__T', bound=org.hipparchus.CalculusFieldElement) # <T>
_pathDelay_2__T = typing.TypeVar('_pathDelay_2__T', bound=org.hipparchus.CalculusFieldElement) # <T>
@typing.overload
diff --git a/org-stubs/orekit/orbits/__init__.pyi b/org-stubs/orekit/orbits/__init__.pyi
index 74e40c26045175cc1e72575910ee9edbc20a95fd..d8a0172479f82245cb140967c2d62ab40f32b596 100644
--- a/org-stubs/orekit/orbits/__init__.pyi
+++ b/org-stubs/orekit/orbits/__init__.pyi
@@ -796,6 +796,9 @@ class FieldOrbit(org.orekit.utils.FieldPVCoordinatesProvider[_FieldOrbit__T], or
Since:
9.0
+
+ Also see:
+ :class:`~org.orekit.orbits.Orbit`
"""
def addKeplerContribution(self, positionAngleType: 'PositionAngleType', t: _FieldOrbit__T, tArray: typing.Union[typing.List[_FieldOrbit__T], jpype.JArray]) -> None:
"""
@@ -874,12 +877,12 @@ class FieldOrbit(org.orekit.utils.FieldPVCoordinatesProvider[_FieldOrbit__T], or
...
def getEquinoctialExDot(self) -> _FieldOrbit__T:
"""
- Get the first component of the equinoctial eccentricity vector.
+ Get the first component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is null.
Returns:
- first component of the equinoctial eccentricity vector
+ first component of the equinoctial eccentricity vector derivative
"""
@@ -896,12 +899,12 @@ class FieldOrbit(org.orekit.utils.FieldPVCoordinatesProvider[_FieldOrbit__T], or
...
def getEquinoctialEyDot(self) -> _FieldOrbit__T:
"""
- Get the second component of the equinoctial eccentricity vector.
+ Get the second component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is null.
Returns:
- second component of the equinoctial eccentricity vector
+ second component of the equinoctial eccentricity vector derivative
"""
@@ -1718,23 +1721,23 @@ class Orbit(org.orekit.time.TimeStamped, org.orekit.time.TimeShiftable['Orbit'],
...
def getEquinoctialEx(self) -> float:
"""
- Get the first component of the equinoctial eccentricity vector derivative.
+ Get the first component of the equinoctial eccentricity vector.
Returns:
- first component of the equinoctial eccentricity vector derivative
+ first component of the equinoctial eccentricity vector
"""
...
def getEquinoctialExDot(self) -> float:
"""
- Get the first component of the equinoctial eccentricity vector.
+ Get the first component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is
:meth:`~org.orekit.orbits.https:.docs.oracle.com.javase.8.docs.api.java.lang.Double.html?is`.
Returns:
- first component of the equinoctial eccentricity vector
+ first component of the equinoctial eccentricity vector derivative
Since:
9.0
@@ -1747,23 +1750,23 @@ class Orbit(org.orekit.time.TimeStamped, org.orekit.time.TimeShiftable['Orbit'],
...
def getEquinoctialEy(self) -> float:
"""
- Get the second component of the equinoctial eccentricity vector derivative.
+ Get the second component of the equinoctial eccentricity vector.
Returns:
- second component of the equinoctial eccentricity vector derivative
+ second component of the equinoctial eccentricity vector
"""
...
def getEquinoctialEyDot(self) -> float:
"""
- Get the second component of the equinoctial eccentricity vector.
+ Get the second component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is
:meth:`~org.orekit.orbits.https:.docs.oracle.com.javase.8.docs.api.java.lang.Double.html?is`.
Returns:
- second component of the equinoctial eccentricity vector
+ second component of the equinoctial eccentricity vector derivative
Since:
9.0
@@ -3143,20 +3146,20 @@ class CartesianOrbit(Orbit):
...
def getEquinoctialEx(self) -> float:
"""
- Get the first component of the equinoctial eccentricity vector derivative.
+ Get the first component of the equinoctial eccentricity vector.
Specified by:
:meth:`~org.orekit.orbits.Orbit.getEquinoctialEx` in class :class:`~org.orekit.orbits.Orbit`
Returns:
- first component of the equinoctial eccentricity vector derivative
+ first component of the equinoctial eccentricity vector
"""
...
def getEquinoctialExDot(self) -> float:
"""
- Get the first component of the equinoctial eccentricity vector.
+ Get the first component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is
:meth:`~org.orekit.orbits.https:.docs.oracle.com.javase.8.docs.api.java.lang.Double.html?is`.
@@ -3165,7 +3168,7 @@ class CartesianOrbit(Orbit):
:meth:`~org.orekit.orbits.Orbit.getEquinoctialExDot` in class :class:`~org.orekit.orbits.Orbit`
Returns:
- first component of the equinoctial eccentricity vector
+ first component of the equinoctial eccentricity vector derivative
Also see:
:meth:`~org.orekit.orbits.Orbit.hasDerivatives`
@@ -3175,20 +3178,20 @@ class CartesianOrbit(Orbit):
...
def getEquinoctialEy(self) -> float:
"""
- Get the second component of the equinoctial eccentricity vector derivative.
+ Get the second component of the equinoctial eccentricity vector.
Specified by:
:meth:`~org.orekit.orbits.Orbit.getEquinoctialEy` in class :class:`~org.orekit.orbits.Orbit`
Returns:
- second component of the equinoctial eccentricity vector derivative
+ second component of the equinoctial eccentricity vector
"""
...
def getEquinoctialEyDot(self) -> float:
"""
- Get the second component of the equinoctial eccentricity vector.
+ Get the second component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is
:meth:`~org.orekit.orbits.https:.docs.oracle.com.javase.8.docs.api.java.lang.Double.html?is`.
@@ -3197,7 +3200,7 @@ class CartesianOrbit(Orbit):
:meth:`~org.orekit.orbits.Orbit.getEquinoctialEyDot` in class :class:`~org.orekit.orbits.Orbit`
Returns:
- second component of the equinoctial eccentricity vector
+ second component of the equinoctial eccentricity vector derivative
Also see:
:meth:`~org.orekit.orbits.Orbit.hasDerivatives`
@@ -3772,20 +3775,20 @@ class CircularOrbit(Orbit, PositionAngleBased):
...
def getEquinoctialEx(self) -> float:
"""
- Get the first component of the equinoctial eccentricity vector derivative.
+ Get the first component of the equinoctial eccentricity vector.
Specified by:
:meth:`~org.orekit.orbits.Orbit.getEquinoctialEx` in class :class:`~org.orekit.orbits.Orbit`
Returns:
- first component of the equinoctial eccentricity vector derivative
+ first component of the equinoctial eccentricity vector
"""
...
def getEquinoctialExDot(self) -> float:
"""
- Get the first component of the equinoctial eccentricity vector.
+ Get the first component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is
:meth:`~org.orekit.orbits.https:.docs.oracle.com.javase.8.docs.api.java.lang.Double.html?is`.
@@ -3794,7 +3797,7 @@ class CircularOrbit(Orbit, PositionAngleBased):
:meth:`~org.orekit.orbits.Orbit.getEquinoctialExDot` in class :class:`~org.orekit.orbits.Orbit`
Returns:
- first component of the equinoctial eccentricity vector
+ first component of the equinoctial eccentricity vector derivative
Also see:
:meth:`~org.orekit.orbits.Orbit.hasDerivatives`
@@ -3804,20 +3807,20 @@ class CircularOrbit(Orbit, PositionAngleBased):
...
def getEquinoctialEy(self) -> float:
"""
- Get the second component of the equinoctial eccentricity vector derivative.
+ Get the second component of the equinoctial eccentricity vector.
Specified by:
:meth:`~org.orekit.orbits.Orbit.getEquinoctialEy` in class :class:`~org.orekit.orbits.Orbit`
Returns:
- second component of the equinoctial eccentricity vector derivative
+ second component of the equinoctial eccentricity vector
"""
...
def getEquinoctialEyDot(self) -> float:
"""
- Get the second component of the equinoctial eccentricity vector.
+ Get the second component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is
:meth:`~org.orekit.orbits.https:.docs.oracle.com.javase.8.docs.api.java.lang.Double.html?is`.
@@ -3826,7 +3829,7 @@ class CircularOrbit(Orbit, PositionAngleBased):
:meth:`~org.orekit.orbits.Orbit.getEquinoctialEyDot` in class :class:`~org.orekit.orbits.Orbit`
Returns:
- second component of the equinoctial eccentricity vector
+ second component of the equinoctial eccentricity vector derivative
Also see:
:meth:`~org.orekit.orbits.Orbit.hasDerivatives`
@@ -4286,20 +4289,20 @@ class EquinoctialOrbit(Orbit, PositionAngleBased):
...
def getEquinoctialEx(self) -> float:
"""
- Get the first component of the equinoctial eccentricity vector derivative.
+ Get the first component of the equinoctial eccentricity vector.
Specified by:
:meth:`~org.orekit.orbits.Orbit.getEquinoctialEx` in class :class:`~org.orekit.orbits.Orbit`
Returns:
- first component of the equinoctial eccentricity vector derivative
+ first component of the equinoctial eccentricity vector
"""
...
def getEquinoctialExDot(self) -> float:
"""
- Get the first component of the equinoctial eccentricity vector.
+ Get the first component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is
:meth:`~org.orekit.orbits.https:.docs.oracle.com.javase.8.docs.api.java.lang.Double.html?is`.
@@ -4308,7 +4311,7 @@ class EquinoctialOrbit(Orbit, PositionAngleBased):
:meth:`~org.orekit.orbits.Orbit.getEquinoctialExDot` in class :class:`~org.orekit.orbits.Orbit`
Returns:
- first component of the equinoctial eccentricity vector
+ first component of the equinoctial eccentricity vector derivative
Also see:
:meth:`~org.orekit.orbits.Orbit.hasDerivatives`
@@ -4318,20 +4321,20 @@ class EquinoctialOrbit(Orbit, PositionAngleBased):
...
def getEquinoctialEy(self) -> float:
"""
- Get the second component of the equinoctial eccentricity vector derivative.
+ Get the second component of the equinoctial eccentricity vector.
Specified by:
:meth:`~org.orekit.orbits.Orbit.getEquinoctialEy` in class :class:`~org.orekit.orbits.Orbit`
Returns:
- second component of the equinoctial eccentricity vector derivative
+ second component of the equinoctial eccentricity vector
"""
...
def getEquinoctialEyDot(self) -> float:
"""
- Get the second component of the equinoctial eccentricity vector.
+ Get the second component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is
:meth:`~org.orekit.orbits.https:.docs.oracle.com.javase.8.docs.api.java.lang.Double.html?is`.
@@ -4340,7 +4343,7 @@ class EquinoctialOrbit(Orbit, PositionAngleBased):
:meth:`~org.orekit.orbits.Orbit.getEquinoctialEyDot` in class :class:`~org.orekit.orbits.Orbit`
Returns:
- second component of the equinoctial eccentricity vector
+ second component of the equinoctial eccentricity vector derivative
Also see:
:meth:`~org.orekit.orbits.Orbit.hasDerivatives`
@@ -4785,7 +4788,7 @@ class FieldCartesianOrbit(FieldOrbit[_FieldCartesianOrbit__T], typing.Generic[_F
...
def getEquinoctialExDot(self) -> _FieldCartesianOrbit__T:
"""
- Get the first component of the equinoctial eccentricity vector.
+ Get the first component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is null.
@@ -4793,7 +4796,7 @@ class FieldCartesianOrbit(FieldOrbit[_FieldCartesianOrbit__T], typing.Generic[_F
:meth:`~org.orekit.orbits.FieldOrbit.getEquinoctialExDot` in class :class:`~org.orekit.orbits.FieldOrbit`
Returns:
- first component of the equinoctial eccentricity vector
+ first component of the equinoctial eccentricity vector derivative
"""
@@ -4813,7 +4816,7 @@ class FieldCartesianOrbit(FieldOrbit[_FieldCartesianOrbit__T], typing.Generic[_F
...
def getEquinoctialEyDot(self) -> _FieldCartesianOrbit__T:
"""
- Get the second component of the equinoctial eccentricity vector.
+ Get the second component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is null.
@@ -4821,7 +4824,7 @@ class FieldCartesianOrbit(FieldOrbit[_FieldCartesianOrbit__T], typing.Generic[_F
:meth:`~org.orekit.orbits.FieldOrbit.getEquinoctialEyDot` in class :class:`~org.orekit.orbits.FieldOrbit`
Returns:
- second component of the equinoctial eccentricity vector
+ second component of the equinoctial eccentricity vector derivative
"""
@@ -5349,7 +5352,7 @@ class FieldCircularOrbit(FieldOrbit[_FieldCircularOrbit__T], PositionAngleBased,
...
def getEquinoctialExDot(self) -> _FieldCircularOrbit__T:
"""
- Get the first component of the equinoctial eccentricity vector.
+ Get the first component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is null.
@@ -5357,7 +5360,7 @@ class FieldCircularOrbit(FieldOrbit[_FieldCircularOrbit__T], PositionAngleBased,
:meth:`~org.orekit.orbits.FieldOrbit.getEquinoctialExDot` in class :class:`~org.orekit.orbits.FieldOrbit`
Returns:
- first component of the equinoctial eccentricity vector
+ first component of the equinoctial eccentricity vector derivative
"""
@@ -5377,7 +5380,7 @@ class FieldCircularOrbit(FieldOrbit[_FieldCircularOrbit__T], PositionAngleBased,
...
def getEquinoctialEyDot(self) -> _FieldCircularOrbit__T:
"""
- Get the second component of the equinoctial eccentricity vector.
+ Get the second component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is null.
@@ -5385,7 +5388,7 @@ class FieldCircularOrbit(FieldOrbit[_FieldCircularOrbit__T], PositionAngleBased,
:meth:`~org.orekit.orbits.FieldOrbit.getEquinoctialEyDot` in class :class:`~org.orekit.orbits.FieldOrbit`
Returns:
- second component of the equinoctial eccentricity vector
+ second component of the equinoctial eccentricity vector derivative
"""
@@ -5828,7 +5831,7 @@ class FieldEquinoctialOrbit(FieldOrbit[_FieldEquinoctialOrbit__T], PositionAngle
...
def getEquinoctialExDot(self) -> _FieldEquinoctialOrbit__T:
"""
- Get the first component of the equinoctial eccentricity vector.
+ Get the first component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is null.
@@ -5836,7 +5839,7 @@ class FieldEquinoctialOrbit(FieldOrbit[_FieldEquinoctialOrbit__T], PositionAngle
:meth:`~org.orekit.orbits.FieldOrbit.getEquinoctialExDot` in class :class:`~org.orekit.orbits.FieldOrbit`
Returns:
- first component of the equinoctial eccentricity vector
+ first component of the equinoctial eccentricity vector derivative
"""
@@ -5856,7 +5859,7 @@ class FieldEquinoctialOrbit(FieldOrbit[_FieldEquinoctialOrbit__T], PositionAngle
...
def getEquinoctialEyDot(self) -> _FieldEquinoctialOrbit__T:
"""
- Get the second component of the equinoctial eccentricity vector.
+ Get the second component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is null.
@@ -5864,7 +5867,7 @@ class FieldEquinoctialOrbit(FieldOrbit[_FieldEquinoctialOrbit__T], PositionAngle
:meth:`~org.orekit.orbits.FieldOrbit.getEquinoctialEyDot` in class :class:`~org.orekit.orbits.FieldOrbit`
Returns:
- second component of the equinoctial eccentricity vector
+ second component of the equinoctial eccentricity vector derivative
"""
@@ -6359,7 +6362,7 @@ class FieldKeplerianOrbit(FieldOrbit[_FieldKeplerianOrbit__T], PositionAngleBase
...
def getEquinoctialExDot(self) -> _FieldKeplerianOrbit__T:
"""
- Get the first component of the equinoctial eccentricity vector.
+ Get the first component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is null.
@@ -6367,7 +6370,7 @@ class FieldKeplerianOrbit(FieldOrbit[_FieldKeplerianOrbit__T], PositionAngleBase
:meth:`~org.orekit.orbits.FieldOrbit.getEquinoctialExDot` in class :class:`~org.orekit.orbits.FieldOrbit`
Returns:
- first component of the equinoctial eccentricity vector
+ first component of the equinoctial eccentricity vector derivative
"""
@@ -6387,7 +6390,7 @@ class FieldKeplerianOrbit(FieldOrbit[_FieldKeplerianOrbit__T], PositionAngleBase
...
def getEquinoctialEyDot(self) -> _FieldKeplerianOrbit__T:
"""
- Get the second component of the equinoctial eccentricity vector.
+ Get the second component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is null.
@@ -6395,7 +6398,7 @@ class FieldKeplerianOrbit(FieldOrbit[_FieldKeplerianOrbit__T], PositionAngleBase
:meth:`~org.orekit.orbits.FieldOrbit.getEquinoctialEyDot` in class :class:`~org.orekit.orbits.FieldOrbit`
Returns:
- second component of the equinoctial eccentricity vector
+ second component of the equinoctial eccentricity vector derivative
"""
@@ -7024,20 +7027,20 @@ class KeplerianOrbit(Orbit, PositionAngleBased):
...
def getEquinoctialEx(self) -> float:
"""
- Get the first component of the equinoctial eccentricity vector derivative.
+ Get the first component of the equinoctial eccentricity vector.
Specified by:
:meth:`~org.orekit.orbits.Orbit.getEquinoctialEx` in class :class:`~org.orekit.orbits.Orbit`
Returns:
- first component of the equinoctial eccentricity vector derivative
+ first component of the equinoctial eccentricity vector
"""
...
def getEquinoctialExDot(self) -> float:
"""
- Get the first component of the equinoctial eccentricity vector.
+ Get the first component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is
:meth:`~org.orekit.orbits.https:.docs.oracle.com.javase.8.docs.api.java.lang.Double.html?is`.
@@ -7046,7 +7049,7 @@ class KeplerianOrbit(Orbit, PositionAngleBased):
:meth:`~org.orekit.orbits.Orbit.getEquinoctialExDot` in class :class:`~org.orekit.orbits.Orbit`
Returns:
- first component of the equinoctial eccentricity vector
+ first component of the equinoctial eccentricity vector derivative
Also see:
:meth:`~org.orekit.orbits.Orbit.hasDerivatives`
@@ -7056,20 +7059,20 @@ class KeplerianOrbit(Orbit, PositionAngleBased):
...
def getEquinoctialEy(self) -> float:
"""
- Get the second component of the equinoctial eccentricity vector derivative.
+ Get the second component of the equinoctial eccentricity vector.
Specified by:
:meth:`~org.orekit.orbits.Orbit.getEquinoctialEy` in class :class:`~org.orekit.orbits.Orbit`
Returns:
- second component of the equinoctial eccentricity vector derivative
+ second component of the equinoctial eccentricity vector
"""
...
def getEquinoctialEyDot(self) -> float:
"""
- Get the second component of the equinoctial eccentricity vector.
+ Get the second component of the equinoctial eccentricity vector derivative.
If the orbit was created without derivatives, the value returned is
:meth:`~org.orekit.orbits.https:.docs.oracle.com.javase.8.docs.api.java.lang.Double.html?is`.
@@ -7078,7 +7081,7 @@ class KeplerianOrbit(Orbit, PositionAngleBased):
:meth:`~org.orekit.orbits.Orbit.getEquinoctialEyDot` in class :class:`~org.orekit.orbits.Orbit`
Returns:
- second component of the equinoctial eccentricity vector
+ second component of the equinoctial eccentricity vector derivative
Also see:
:meth:`~org.orekit.orbits.Orbit.hasDerivatives`
diff --git a/org-stubs/orekit/propagation/analytical/intelsat/__init__.pyi b/org-stubs/orekit/propagation/analytical/intelsat/__init__.pyi
index cf03069115c9fdbbe691bc02016b300cdf4316e8..12e3379540355c3a8683c6b9a0aa907ac071320a 100644
--- a/org-stubs/orekit/propagation/analytical/intelsat/__init__.pyi
+++ b/org-stubs/orekit/propagation/analytical/intelsat/__init__.pyi
@@ -187,6 +187,7 @@ class FieldIntelsatElevenElementsPropagator(org.orekit.propagation.analytical.Fi
"""
...
def getGeocentricLatitudeDegrees(self) -> org.hipparchus.analysis.differentiation.FieldUnivariateDerivative2[_FieldIntelsatElevenElementsPropagator__T]: ...
+ def getIntelsatElevenElements(self) -> FieldIntelsatElevenElements[_FieldIntelsatElevenElementsPropagator__T]: ...
def getOrbitRadius(self) -> org.hipparchus.analysis.differentiation.FieldUnivariateDerivative2[_FieldIntelsatElevenElementsPropagator__T]: ...
def getParametersDrivers(self) -> java.util.List[org.orekit.utils.ParameterDriver]: ...
def propagateInEcef(self, fieldAbsoluteDate: org.orekit.time.FieldAbsoluteDate[_FieldIntelsatElevenElementsPropagator__T]) -> org.orekit.utils.FieldPVCoordinates[_FieldIntelsatElevenElementsPropagator__T]: ...
@@ -417,6 +418,16 @@ class IntelsatElevenElementsPropagator(org.orekit.propagation.analytical.Abstrac
the satellite's geocentric latitude in degrees
+ """
+ ...
+ def getIntelsatElevenElements(self) -> IntelsatElevenElements:
+ """
+ Get the Intelsat's 11 elements used by the propagator.
+
+ Returns:
+ the Intelsat's 11 elements used by the propagator
+
+
"""
...
def getOrbitRadius(self) -> org.hipparchus.analysis.differentiation.UnivariateDerivative2:
diff --git a/org-stubs/orekit/propagation/events/__init__.pyi b/org-stubs/orekit/propagation/events/__init__.pyi
index 2b2e8b78ed93e2cf1de6cd1fecbf0d735302c8df..0a99b97b1f2d3cc78714c03eeb7a4f482df8d097 100644
--- a/org-stubs/orekit/propagation/events/__init__.pyi
+++ b/org-stubs/orekit/propagation/events/__init__.pyi
@@ -5479,7 +5479,7 @@ class PositionAngleDetector(AbstractDetector['PositionAngleDetector']):
:meth:`~org.orekit.orbits.OrbitType.CIRCULAR` orbits, or longitude argument for
:meth:`~org.orekit.orbits.OrbitType.EQUINOCTIAL` orbits. It does not support
:meth:`~org.orekit.orbits.OrbitType.CARTESIAN` orbits. The angles can be either
- :meth:`~org.orekit.orbits.PositionAngleType.TRUE`, {link :meth:`~org.orekit.orbits.PositionAngleType.MEAN` or
+ :meth:`~org.orekit.orbits.PositionAngleType.TRUE`, :meth:`~org.orekit.orbits.PositionAngleType.MEAN` or
:meth:`~org.orekit.orbits.PositionAngleType.ECCENTRIC` angles.
Since: