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OREKIT (ORbits Extrapolation KIT) is a low level space dynamics library. It provides basic elements (orbits, dates, attitude, frames ...) and various algorithms to handle them (conversions, analytical and numerical propagation, pointing ...).

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/* Copyright 2002-2019 CS Systèmes d'Information
 * Licensed to CS Systèmes d'Information (CS) under one or more
 * contributor license agreements.  See the NOTICE file distributed with
 * this work for additional information regarding copyright ownership.
 * CS licenses this file to You under the Apache License, Version 2.0
 * (the "License"); you may not use this file except in compliance with
 * the License.  You may obtain a copy of the License at
 *
 *   http://www.apache.org/licenses/LICENSE-2.0
 *
 * Unless required by applicable law or agreed to in writing, software
 * distributed under the License is distributed on an "AS IS" BASIS,
 * WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
 * See the License for the specific language governing permissions and
 * limitations under the License.
 */
package org.orekit.frames;

import org.hipparchus.RealFieldElement;
import org.orekit.time.AbsoluteDate;
import org.orekit.time.FieldAbsoluteDate;
import org.orekit.utils.PVCoordinatesProvider;

/** Class for frames moving with an orbiting satellite.
 *
 * 

There are several local orbital frames available. They are specified * by the {@link LOFType} enumerate.

* *

Do not use the {@link #getTransformTo(Frame, FieldAbsoluteDate)} method as it is * not implemented. * * @author Luc Maisonobe * @see org.orekit.propagation.SpacecraftState#toTransform() */ public class LocalOrbitalFrame extends Frame { /** Serializable UID. */ private static final long serialVersionUID = -4469440345574964950L; /** Build a new instance. * *

It is highly recommended that {@code provider} use an analytic formulation and * not numerical integration as large integration errors may result from many short * propagations. * * @param parent parent frame (must be non-null) * @param type frame type * @param provider provider used to compute frame motion. * @param name name of the frame * @exception IllegalArgumentException if the parent frame is null */ public LocalOrbitalFrame(final Frame parent, final LOFType type, final PVCoordinatesProvider provider, final String name) throws IllegalArgumentException { super(parent, new LocalProvider(type, provider, parent, name), name, false); } /** Local provider for transforms. */ private static class LocalProvider implements TransformProvider { /** Serializable UID. */ private static final long serialVersionUID = 20170421L; /** Frame type. */ private final LOFType type; /** Provider used to compute frame motion. */ private final PVCoordinatesProvider provider; /** Reference frame. */ private final Frame reference; /** Name of the frame. */ private final String name; /** Simple constructor. * @param type frame type * @param provider provider used to compute frame motion * @param reference reference frame * @param name name of the frame */ LocalProvider(final LOFType type, final PVCoordinatesProvider provider, final Frame reference, final String name) { this.type = type; this.provider = provider; this.reference = reference; this.name = name; } /** {@inheritDoc} */ public Transform getTransform(final AbsoluteDate date) { return type.transformFromInertial(date, provider.getPVCoordinates(date, reference)); } /** * This method is not implemented. * *

{@inheritDoc} * * @throws UnsupportedOperationException always. */ public > FieldTransform getTransform( final FieldAbsoluteDate date) throws UnsupportedOperationException { throw new UnsupportedOperationException( "FieldTransforms are not supported for a LocalOrbitalFrame: " + name + ". Please contact [email protected] if you " + "would like to add this feature."); } } }





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