/** @param args */
public static void main(String[] args) {
try {
// force dot as decimal separator
Locale.setDefault(new Locale("en", "US"));
// Get current time
long start = System.currentTimeMillis();
RinexNavigation navigationIn =
new RinexNavigation(RinexNavigation.IGN_NAVIGATION_HOURLY_ZIM2);
FileInputStream fis = new FileInputStream(".\\data\\aphemeris.dat");
// FileInputStream fis = new FileInputStream(".\\data\\assistnow.dat");
DataInputStream dis = new DataInputStream(fis);
String msg = null;
try {
msg = dis.readUTF();
while (msg != null) {
System.out.println("Msg:[" + msg + "]");
if (msg.equalsIgnoreCase(Streamable.MESSAGE_OBSERVATIONS)) {
Observations o = new Observations(dis, false);
} else if (msg.equalsIgnoreCase(Streamable.MESSAGE_EPHEMERIS)) {
EphGps eph1 = new EphGps(dis, false);
System.out.println(
"found sat" + eph1.getSatID() + " time:" + eph1.getRefTime().getGpsTime());
EphGps eph2 =
navigationIn.findEph(
eph1.getRefTime().getMsec(), eph1.getSatID(), eph1.getSatType());
// Compare
if (eph2 != null) {
double ms = eph1.getRefTime().getGpsTime() - eph2.getRefTime().getGpsTime();
System.out.println(" time dif:" + (ms / 1000) + "s " + (ms % 1000) + "ms");
;
equalDouble("Af0", eph1.getAf0(), eph2.getAf0());
equalDouble("Af1", eph1.getAf1(), eph2.getAf1());
equalDouble("Af2", eph1.getAf2(), eph2.getAf2());
equalDouble("Cic", eph1.getCic(), eph2.getCic());
equalDouble("Cis", eph1.getCis(), eph2.getCis());
equalDouble("Crc", eph1.getCrc(), eph2.getCrc());
equalDouble("Crs", eph1.getCrs(), eph2.getCrs());
equalDouble("Cuc", eph1.getCuc(), eph2.getCuc());
equalDouble("Cus", eph1.getCus(), eph2.getCus());
equalDouble("DeltaN", eph1.getDeltaN(), eph2.getDeltaN());
equalDouble("E", eph1.getE(), eph2.getE());
equalDouble("FitInt", eph1.getFitInt(), eph2.getFitInt());
equalDouble("I0", eph1.getI0(), eph2.getI0());
equalDouble("iDot", eph1.getiDot(), eph2.getiDot());
equalDouble("M0", eph1.getM0(), eph2.getM0());
equalDouble("Omega", eph1.getOmega(), eph2.getOmega());
equalDouble("Omega0", eph1.getOmega0(), eph2.getOmega0());
equalDouble("OmegaDot", eph1.getOmegaDot(), eph2.getOmegaDot());
equalDouble("RootA", eph1.getRootA(), eph2.getRootA());
equalDouble("Tgd", eph1.getTgd(), eph2.getTgd());
equalDouble("Toc", eph1.getToc(), eph2.getToc());
equalDouble("Toe", eph1.getToe(), eph2.getToe());
equalDouble("Iodc", eph1.getIodc(), eph2.getIodc());
equalDouble("Iode", eph1.getIode(), eph2.getIode());
equalDouble("L2Code", eph1.getL2Code(), eph2.getL2Code());
equalDouble("L2Flag", eph1.getL2Flag(), eph2.getL2Flag());
equalDouble("SvAccur", eph1.getSvAccur(), eph2.getSvAccur());
equalDouble("SvHealth", eph1.getSvHealth(), eph2.getSvHealth());
} else {
System.out.println(
"EPH 2 not found for " + eph1.getSatID() + " at " + eph1.getRefTime());
}
} else if (msg.equalsIgnoreCase(Streamable.MESSAGE_OBSERVATIONS_SET)) {
ObservationSet eps = new ObservationSet(dis, false);
// nothing to do with ?
} else if (msg.equalsIgnoreCase(Streamable.MESSAGE_IONO)) {
IonoGps iono = new IonoGps(dis, false);
// addIonospheric(iono);
} else if (msg.equalsIgnoreCase(Streamable.MESSAGE_COORDINATES)) {
Coordinates c = Coordinates.readFromStream(dis, false);
// setDefinedPosition(c);
} else {
System.out.println("Unknow Msg:[" + msg + "]");
}
msg = dis.readUTF();
}
} catch (EOFException eof) {
// ok
}
fis.close();
try {
navigationIn.release(true, 10000);
} catch (InterruptedException ie) {
ie.printStackTrace();
}
// Get and display elapsed time
int elapsedTimeSec = (int) Math.floor((System.currentTimeMillis() - start) / 1000);
int elapsedTimeMillisec =
(int) ((System.currentTimeMillis() - start) - elapsedTimeSec * 1000);
System.out.println(
"\nElapsed time (read + proc + display + write): "
+ elapsedTimeSec
+ " seconds "
+ elapsedTimeMillisec
+ " milliseconds.");
} catch (Exception e) {
e.printStackTrace();
}
}
