Example #1
0
  public void readOrbitData() throws IOException {

    if (_productFile instanceof DorisOrbitProductFile) {

      final DorisOrbitProductFile dorisProdFile = (DorisOrbitProductFile) _productFile;
      final Record orbitRecord = dorisProdFile.readOrbitData();

      OrbitVector orb = null;
      final SimpleDateFormat dateFormat = new SimpleDateFormat("dd-MMM-yyyy HH:mm:ss.SSSSSS");
      final ArrayList<OrbitVector> orbitVectorList = new ArrayList<OrbitVector>();

      final int numFields = orbitRecord.getNumFields();
      for (int i = 0; i < numFields; ++i) {

        final Field f = orbitRecord.getFieldAt(i);

        final String fieldName = f.getName();
        if (fieldName.contains("blank")) {
          continue;
        } else if (fieldName.contains("utc_time")) {
          orb = new OrbitVector();
          try {
            orb.utcTime = ProductData.UTC.parse(f.getData().getElemString()).getMJD();
          } catch (ParseException e) {
            throw new IllegalFileFormatException("Failed to parse UTC time " + e.getMessage());
          }
        } else if (fieldName.contains("delta_ut1")) {
          if (orb != null) orb.delta_ut1 = Double.parseDouble(f.getData().getElemString());
        } else if (fieldName.contains("abs_orbit")) {
          if (orb != null)
            orb.absOrbit = Integer.parseInt(f.getData().getElemString().replace("+", ""));
        } else if (fieldName.contains("x_pos")) {
          if (orb != null) orb.xPos = Double.parseDouble(f.getData().getElemString());
        } else if (fieldName.contains("y_pos")) {
          if (orb != null) orb.yPos = Double.parseDouble(f.getData().getElemString());
        } else if (fieldName.contains("z_pos")) {
          if (orb != null) orb.zPos = Double.parseDouble(f.getData().getElemString());
        } else if (fieldName.contains("x_vel")) {
          if (orb != null) orb.xVel = Double.parseDouble(f.getData().getElemString());
        } else if (fieldName.contains("y_vel")) {
          if (orb != null) orb.yVel = Double.parseDouble(f.getData().getElemString());
        } else if (fieldName.contains("z_vel")) {
          if (orb != null) orb.zVel = Double.parseDouble(f.getData().getElemString());
        } else if (fieldName.contains("qual_flags")) {
          if (orb != null) orb.qualFlags = f.getData().getElemString();
          orbitVectorList.add(orb);
        }
      }

      dataRecords = orbitVectorList.toArray(new OrbitVector[orbitVectorList.size()]);

      recordTimes = new double[dataRecords.length];
      for (int i = 0; i < dataRecords.length; i++) {
        recordTimes[i] = dataRecords[i].utcTime;
      }
    }
  }
Example #2
0
  /**
   * Get orbit vector for given UTC time.
   *
   * @param utc The UTC time
   * @throws Exception for incorrect time
   * @return The orbit vector
   */
  public OrbitVector getOrbitVector(double utc) throws Exception {

    final int interpOrder = 8;
    final int nRecords = recordTimes.length;
    double t0 = recordTimes[0];
    double tN = recordTimes[nRecords - 1];

    // final int n = Arrays.binarySearch(recordTimes, utc);
    // binary search not needed, we can pre-compute index for given utc wrt delta, and start/end
    // time
    final double tRel = (utc - t0) / (tN - t0) * (nRecords - 1); // data index from 0
    final int itRel =
        (int)
            Math.max(
                1, Math.min(Math.round(tRel) - (interpOrder / 2), (nRecords - 1) - interpOrder));

    // indices for populating arrays - Working with 8th Order => 9 points
    final int n0 = itRel;
    final int n1 = itRel + 1;
    final int n2 = itRel + 2;
    final int n3 = itRel + 3;
    final int n4 = itRel + 4; // <- closest to interpolation point
    final int n5 = itRel + 5;
    final int n6 = itRel + 6;
    final int n7 = itRel + 7;
    final int n8 = itRel + 8;

    // TODO: Verify validity of check for incorrect UTC time in parsing orbit
    // ....I'm not sure that this check is very smart, and that it would pick up not fully
    // overlapping arc
    if (n0 < 0
        || n1 < 0
        || n2 < 0
        || n3 < 0
        || n4 < 0
        || n5 > nRecords
        || n6 > nRecords
        || n7 > nRecords
        || n8 > nRecords) {
      throw new Exception("Incorrect UTC time");
    }

    final double[] delta_ut1Array = {
      dataRecords[n0].delta_ut1,
      dataRecords[n1].delta_ut1,
      dataRecords[n2].delta_ut1,
      dataRecords[n3].delta_ut1,
      dataRecords[n4].delta_ut1,
      dataRecords[n5].delta_ut1,
      dataRecords[n6].delta_ut1,
      dataRecords[n7].delta_ut1,
      dataRecords[n8].delta_ut1
    };

    final double[] xPosArray = {
      dataRecords[n0].xPos,
      dataRecords[n1].xPos,
      dataRecords[n2].xPos,
      dataRecords[n3].xPos,
      dataRecords[n4].xPos,
      dataRecords[n5].xPos,
      dataRecords[n6].xPos,
      dataRecords[n7].xPos,
      dataRecords[n8].xPos
    };

    final double[] yPosArray = {
      dataRecords[n0].yPos,
      dataRecords[n1].yPos,
      dataRecords[n2].yPos,
      dataRecords[n3].yPos,
      dataRecords[n4].yPos,
      dataRecords[n5].yPos,
      dataRecords[n6].yPos,
      dataRecords[n7].yPos,
      dataRecords[n8].yPos
    };

    final double[] zPosArray = {
      dataRecords[n0].zPos,
      dataRecords[n1].zPos,
      dataRecords[n2].zPos,
      dataRecords[n3].zPos,
      dataRecords[n4].zPos,
      dataRecords[n5].zPos,
      dataRecords[n6].zPos,
      dataRecords[n7].zPos,
      dataRecords[n8].zPos
    };

    final double[] xVelArray = {
      dataRecords[n0].xVel,
      dataRecords[n1].xVel,
      dataRecords[n2].xVel,
      dataRecords[n3].xVel,
      dataRecords[n4].xVel,
      dataRecords[n5].xVel,
      dataRecords[n6].xVel,
      dataRecords[n7].xVel,
      dataRecords[n8].xVel
    };

    final double[] yVelArray = {
      dataRecords[n0].yVel,
      dataRecords[n1].yVel,
      dataRecords[n2].yVel,
      dataRecords[n3].yVel,
      dataRecords[n4].yVel,
      dataRecords[n5].yVel,
      dataRecords[n6].yVel,
      dataRecords[n7].yVel,
      dataRecords[n8].yVel
    };

    final double[] zVelArray = {
      dataRecords[n0].zVel,
      dataRecords[n1].zVel,
      dataRecords[n2].zVel,
      dataRecords[n3].zVel,
      dataRecords[n4].zVel,
      dataRecords[n5].zVel,
      dataRecords[n6].zVel,
      dataRecords[n7].zVel,
      dataRecords[n8].zVel
    };

    final OrbitVector orb = new OrbitVector();

    double ref = tRel - itRel;

    orb.utcTime = utc;
    orb.absOrbit = dataRecords[n1].absOrbit;
    orb.qualFlags = dataRecords[n1].qualFlags;
    orb.delta_ut1 = lagrangeEightOrderInterpolation(delta_ut1Array, ref);
    orb.xPos = lagrangeEightOrderInterpolation(xPosArray, ref);
    orb.yPos = lagrangeEightOrderInterpolation(yPosArray, ref);
    orb.zPos = lagrangeEightOrderInterpolation(zPosArray, ref);
    orb.xVel = lagrangeEightOrderInterpolation(xVelArray, ref);
    orb.yVel = lagrangeEightOrderInterpolation(yVelArray, ref);
    orb.zVel = lagrangeEightOrderInterpolation(zVelArray, ref);
    /*
    final double dt = (utc - recordTimes[n1]) / (recordTimes[n2] - recordTimes[n1]);
    final double w0 = w(dt + 1.0);
    final double w1 = w(dt);
    final double w2 = w(1.0 - dt);
    final double w3 = w(2.0 - dt);

    final OrbitVector orb = new OrbitVector();
    orb.utcTime = utc;
    orb.absOrbit = dataRecords[n1].absOrbit;
    orb.qualFlags = dataRecords[n1].qualFlags;

    orb.delta_ut1 = w0*dataRecords[n0].delta_ut1 +
                    w1*dataRecords[n1].delta_ut1 +
                    w2*dataRecords[n2].delta_ut1 +
                    w3*dataRecords[n3].delta_ut1;

    orb.xPos = w0*dataRecords[n0].xPos +
               w1*dataRecords[n1].xPos +
               w2*dataRecords[n2].xPos +
               w3*dataRecords[n3].xPos;

    orb.yPos = w0*dataRecords[n0].yPos +
               w1*dataRecords[n1].yPos +
               w2*dataRecords[n2].yPos +
               w3*dataRecords[n3].yPos;

    orb.zPos = w0*dataRecords[n0].zPos +
               w1*dataRecords[n1].zPos +
               w2*dataRecords[n2].zPos +
               w3*dataRecords[n3].zPos;

    orb.xVel = w0*dataRecords[n0].xVel +
               w1*dataRecords[n1].xVel +
               w2*dataRecords[n2].xVel +
               w3*dataRecords[n3].xVel;

    orb.yVel = w0*dataRecords[n0].yVel +
               w1*dataRecords[n1].yVel +
               w2*dataRecords[n2].yVel +
               w3*dataRecords[n3].yVel;

    orb.zVel = w0*dataRecords[n0].zVel +
               w1*dataRecords[n1].zVel +
               w2*dataRecords[n2].zVel +
               w3*dataRecords[n3].zVel;
    */
    return orb;
  }