QZSSOrbitalElements.java
/* Copyright 2002-2020 CS GROUP
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*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
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package org.orekit.propagation.analytical.gnss;
/** This interface provides the minimal set of orbital elements needed by the {@link QZSSPropagator}.
*
* @see <a href="http://qzss.go.jp/en/technical/download/pdf/ps-is-qzss/is-qzss-pnt-003.pdf?t=1549268771755">
* QZSS Interface Specification</a>
*
* @author Bryan Cazabonne
* @since 10.0
*
*/
public interface QZSSOrbitalElements extends GNSSOrbitalElements {
// Constants
/** WGS 84 value of the Earth's universal gravitational parameter for QZSS user in m³/s². */
double QZSS_MU = 3.986005e+14;
/** Value of Pi for conversion from semicircles to radian. */
double QZSS_PI = 3.1415926535898;
/** Duration of the QZSS week in seconds. */
double QZSS_WEEK_IN_SECONDS = 604800.;
/** Number of weeks in the QZSS cycle. */
int QZSS_WEEK_NB = 1024;
/**
* Gets the Issue Of Data Clock (IODC).
*
* @return the Issue Of Data Clock (IODC)
*/
default int getIODC() {
return 0;
}
/**
* Gets the Issue Of Data Ephemeris (IODE).
*
* @return the Issue Of Data Ephemeris (IODE)
*/
default int getIODE() {
return 0;
}
/**
* Gets the estimated group delay differential TGD between SV clock and L1C/A.
*
* @return the estimated group delay differential TGD between SV clock and L1C/A (s)
*/
default double getTGD() {
return 0.0;
}
}