IRNSSOrbitalElements.java
/* Copyright 2002-2020 CS GROUP
* Licensed to CS GROUP (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.propagation.analytical.gnss;
/** This interface provides the minimal set of orbital elements needed by the {@link IRNSSPropagator}.
*
* @see "Indian Regiona Navigation Satellite System, Signal In Space ICD
* for standard positioning service, version 1.1"
*
* @author Bryan Cazabonne
* @since 10.1
*
*/
public interface IRNSSOrbitalElements extends GNSSOrbitalElements {
/** WGS 84 value of the Earth's universal gravitational parameter for IRNSS user in m³/s². */
double IRNSS_MU = 3.986005e+14;
/** Value of Pi for conversion from semicircles to radian. */
double IRNSS_PI = 3.1415926535898;
/** Duration of the IRNSS week in seconds. */
double IRNSS_WEEK_IN_SECONDS = 604800.;
/** Number of weeks in the IRNSS cycle. */
int IRNSS_WEEK_NB = 1024;
/**
* Gets the Issue Of Data Ephemeris and Clock (IODEC).
*
* @return the Issue Of Data Ephemeris and Clock (IODEC)
*/
default int getIODEC() {
return 0;
}
/**
* Gets the estimated group delay differential TGD for L5-S correction.
*
* @return the estimated group delay differential TGD for L5-S correction (s)
*/
default double getTGD() {
return 0.0;
}
}