STK Components for Java 2022 r2

## Reference Frames and Transformations |

This topic builds upon the foundation of geometrical and coordinate primitives discussed in the
Axes, Points, and Vectors and Coordinates topics.
To begin, we define the geometrical concept of a
ReferenceFrame
as a location point (origin) and a set of axes. A common example of a reference frame is the Earth's fixed frame,
**EarthCentralBody.FixedFrame** (get / set).
In this frame, the
Point
defining the origin is at the center of mass of the Earth and the
Axes are
aligned such that (in Cartesian coordinates) the Z-axis is pointed North and the X-axis intersects the surface
at 0 latitude, 0 longitude. The Y-axis is then defined by the right-hand rule.

Transforming Geometry

GeometryTransformer allows you to easily transform between geometry components by following the chain of relationships between them. One of the primary uses of the transformer is to allow the user to switch between two reference frames. The following example shows how to obtain an evaluator for the transformation between the Earth fixed and Earth inertial reference frames and use it to find an equivalent inertial vector for a given fixed vector:

Java

// Get the Earth central body and assign Earth Orientation Parameters loaded from // the specified EOP data file. EarthCentralBody earth = CentralBodiesFacet.getFromContext().getEarth(); earth.setOrientationParameters(EarthOrientationParametersFile.readData(eopPath)); // Get an evaluator to transform from the fixed to inertial frames, and evaluate it // at 'now' to get the actual transformation. ReferenceFrameEvaluator evaluator = GeometryTransformer.getReferenceFrameTransformation(earth.getFixedFrame(), earth.getInertialFrame()); KinematicTransformation transformation = evaluator.evaluate(JulianDate.getNow(), 0); // Use the transformation to transform a vector in the fixed frame to the inertial frame. Cartesian fixedVectorToTransform = new Cartesian(1.0, 2.0, 3.0); Cartesian equivalentInertialVector = transformation.transform(fixedVectorToTransform);

Each geometry component is defined relative to another geometry component. A
Point is defined in a
ReferenceFrame. A
Vector is defined in a set of
Axes. A set of
Axes or a
ReferenceFrame is defined in terms of another set of
Axes or a
ReferenceFrame, respectively. However, each
Point
is not necessarily defined in terms of the same
ReferenceFrame
all the time. For example, the
Point representing a spacecraft traveling
toward the Moon may initially be defined in an Earth-centered
ReferenceFrame.
As it gets closer to the Moon, it may switch to a Moon-centered
ReferenceFrame.
To handle this, the geometry components' evaluators have a property called
**DefinedInIntervals** (get)
which identifies the
ReferenceFrame or
Axes in which the component is defined
over that interval. In the case of the interplanetary trajectory, the
**DefinedInIntervals** (get)
collection contains two
TimeInterval<ReferenceFrame> objects.
The first holds the Earth-centered
ReferenceFrame in its
**Data** (get) property, and the second holds the Moon-centered
ReferenceFrame as its
**Data** (get).
The first interval stops at the same time the second interval starts, with the
**IsStartIncluded** (get) and
**IsStopIncluded** (get) properties of the
TimeInterval<ReferenceFrame> indicating which system is
used at that time. This allows a single geometry component to be defined in different systems at different times.

In general, it is best to use the
GeometryTransformer
to observe the geometry in the desired system. However, to find the
Axes or
ReferenceFrame
in which a component is defined at a given time, call the
findIntervalContainingDate
method with the
JulianDate used to evaluate the component.
Then, get the
**Data** (get) property of the
TimeInterval<T>.

Each geometry component knows how to evaluate itself with respect to the components held in
**DefinedInIntervals** (get). For example, if a
PointEvaluator is defined in the Earth fixed frame, then calling
evaluate
will return the position and its derivatives with respect to the Earth fixed frame.
To obtain the position, velocity, acceleration, etc. with respect to the Earth inertial frame instead, use the
GeometryTransformer.observePoint
method, as shown in the next example.

Java

// Get the Earth central body and assign Earth Orientation Parameters loaded from // the specified EOP data file. EarthCentralBody earth = CentralBodiesFacet.getFromContext().getEarth(); earth.setOrientationParameters(EarthOrientationParametersFile.readData(eopPath)); // Create a point at a fixed location with respect to the Earth fixed reference frame. PointFixedOffset point = new PointFixedOffset(earth.getFixedFrame(), new Cartesian(8000000.0, 0.0, 0.0)); // Get an evaluator which can transform the point into the Earth inertial // reference frame at a given time. PointEvaluator evaluator = GeometryTransformer.observePoint(point, earth.getInertialFrame()); // Evaluate the evaluator 'now'. The point is stationary with respect to the fixed frame, but // it is moving with respect to the inertial frame. Motion1<Cartesian> positionAndVelocity = evaluator.evaluate(JulianDate.getNow(), 1);

For a Point, the
GeometryTransformer follows the chains created by the
ReferenceFrame in the
**DefinedInIntervals** (get)
to determine the shortest sequence of transformations between any two geometry components. In general,
whenever creating an evaluator to evaluate vector geometry, it is best to get the evaluator through the
GeometryTransformer rather than calling
getEvaluator
on a particular geometry component itself. This ensures that the evaluator computes the geometry in the expected reference system.

Lastly, new geometry components can be easily added by deriving from Axes, Point, or Vector and creating the corresponding AxesEvaluator, PointEvaluator, or VectorEvaluator respectively. These user-defined components can then participate in GeometryTransformer transformations and other geometry types just like the existing components included with STK Components.

The geometry components can be found in the agi.foundation.geometry package.