X-Git-Url: https://git.gag.com/?p=fw%2Faltos;a=blobdiff_plain;f=altoslib%2FAltosEepromMega.java;h=1616de771ef2cdbdcea4b6607a2f88549968ffbf;hp=b85c04bffc576559061949a2d3e879b4d9685a7d;hb=b8fa4e9a077e8e04b922d0c434c139ad0a57ee66;hpb=d203a2da2641bec21a4257c8a7b03d9a1eba53a5

diff --git a/altoslib/AltosEepromMega.java b/altoslib/AltosEepromMega.java
index b85c04bf..1616de77 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_5;
 
 import java.io.*;
 import java.util.*;
@@ -24,13 +24,20 @@ 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 */
 	public int flight() { return data16(0); }
 	public int ground_accel() { return data16(2); }
 	public int ground_pres() { return data32(4); }
-	public int ground_temp() { return data32(8); }
+	public int ground_accel_along() { return data16(8); }
+	public int ground_accel_across() { return data16(10); }
+	public int ground_accel_through() { return data16(12); }
+	public int ground_roll() { return data16(14); }
+	public int ground_pitch() { return data16(16); }
+	public int ground_yaw() { return data16(18); }
 
 	/* AO_LOG_STATE elements */
 	public int state() { return data16(0); }
@@ -68,7 +75,14 @@ public class AltosEepromMega extends AltosEeprom {
 	public int year() { return data8(14); }
 	public int month() { return data8(15); }
 	public int day() { return data8(16); }
-	
+	public int course() { return data8(17); }
+	public int ground_speed() { return data16(18); }
+	public int climb_rate() { return data16(20); }
+	public int pdop() { return data8(22); }
+	public int hdop() { return data8(23); }
+	public int vdop() { return data8(24); }
+	public int mode() { return data8(25); }
+
 	/* AO_LOG_GPS_SAT elements */
 	public int nsat() { return data16(0); }
 	public int svid(int n) { return data8(2 + n * 2); }
@@ -104,7 +118,6 @@ public class AltosEepromMega extends AltosEeprom {
 			state.set_flight(flight());
 			state.set_ground_accel(ground_accel());
 			state.set_ground_pressure(ground_pres());
-			state.set_temperature(ground_temp() / 100.0);
 			break;
 		case AltosLib.AO_LOG_STATE:
 			state.set_tick(tick);
@@ -115,19 +128,19 @@ 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;
 
@@ -148,6 +161,7 @@ public class AltosEepromMega extends AltosEeprom {
 				voltages[i] = AltosConvert.mega_pyro_voltage(sense(i));
 
 			state.set_ignitor_voltage(voltages);
+			state.set_pyro_fired(pyro());
 			break;
 		case AltosLib.AO_LOG_GPS_TIME:
 			state.set_tick(tick);
@@ -170,12 +184,32 @@ public class AltosEepromMega extends AltosEeprom {
 			gps.year = 2000 + year();
 			gps.month = month();
 			gps.day = day();
+			gps.ground_speed = ground_speed() * 1.0e-2;
+			gps.course = course() * 2;
+			gps.climb_rate = climb_rate() * 1.0e-2;
+			if (state.compare_version("1.4.9") >= 0) {
+				gps.pdop = pdop() / 10.0;
+				gps.hdop = hdop() / 10.0;
+				gps.vdop = vdop() / 10.0;
+			} else {
+				gps.pdop = pdop() / 100.0;
+				if (gps.pdop < 0.8)
+					gps.pdop += 2.56;
+				gps.hdop = hdop() / 100.0;
+				if (gps.hdop < 0.8)
+					gps.hdop += 2.56;
+				gps.vdop = vdop() / 100.0;
+				if (gps.vdop < 0.8)
+					gps.vdop += 2.56;
+			}
 			break;
 		case AltosLib.AO_LOG_GPS_SAT:
 			state.set_tick(tick);
 			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;