X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=altoslib%2FAltosEepromMega.java;h=b8a1b9e86dc61ad09403b33c9de4ec54274a3150;hb=f750ef6f9745b15af45bb80f5b46b9e6f51796d8;hp=bccfc62103b947044365b364412ce236aada0ae5;hpb=528e2e41112cad8a81bccbb89c3bd202b818a506;p=fw%2Faltos diff --git a/altoslib/AltosEepromMega.java b/altoslib/AltosEepromMega.java index bccfc621..b8a1b9e8 100644 --- a/altoslib/AltosEepromMega.java +++ b/altoslib/AltosEepromMega.java @@ -15,7 +15,7 @@ * 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA. */ -package org.altusmetrum.altoslib_1; +package org.altusmetrum.altoslib_3; import java.io.*; import java.util.*; @@ -24,6 +24,8 @@ import java.text.*; public class AltosEepromMega extends AltosEeprom { public static final int record_length = 32; + public static final int max_sat = 12; + public int record_length() { return record_length; } /* AO_LOG_FLIGHT elements */ @@ -115,19 +117,19 @@ public class AltosEepromMega extends AltosEeprom { state.set_ms5607(pres(), temp()); AltosIMU imu = new AltosIMU(); - imu.accel_x = accel_x(); - imu.accel_y = accel_y(); - imu.accel_z = accel_z(); + imu.accel_x = AltosIMU.convert_accel(accel_x()); + imu.accel_y = AltosIMU.convert_accel(accel_y()); + imu.accel_z = AltosIMU.convert_accel(accel_z()); - imu.gyro_x = gyro_x(); - imu.gyro_y = gyro_y(); - imu.gyro_z = gyro_z(); + imu.gyro_x = AltosIMU.convert_gyro(gyro_x()); + imu.gyro_y = AltosIMU.convert_gyro(gyro_y()); + imu.gyro_z = AltosIMU.convert_gyro(gyro_z()); state.imu = imu; AltosMag mag = new AltosMag(); - mag.x = mag_x(); - mag.y = mag_y(); - mag.z = mag_z(); + mag.x = AltosMag.convert_gauss(mag_x()); + mag.y = AltosMag.convert_gauss(mag_y()); + mag.z = AltosMag.convert_gauss(mag_z()); state.mag = mag; @@ -167,7 +169,7 @@ public class AltosEepromMega extends AltosEeprom { gps.nsat = (flags & AltosLib.AO_GPS_NUM_SAT_MASK) >> AltosLib.AO_GPS_NUM_SAT_SHIFT; - gps.year = year(); + gps.year = 2000 + year(); gps.month = month(); gps.day = day(); break; @@ -176,6 +178,8 @@ public class AltosEepromMega extends AltosEeprom { gps = state.make_temp_gps(true); int n = nsat(); + if (n > max_sat) + n = max_sat; for (int i = 0; i < n; i++) gps.add_sat(svid(i), c_n(i)); break;