altosui: Support MM telemetry packets
[fw/altos] / altoslib / AltosRecordTM.java
diff --git a/altoslib/AltosRecordTM.java b/altoslib/AltosRecordTM.java
new file mode 100644 (file)
index 0000000..afb7079
--- /dev/null
@@ -0,0 +1,199 @@
+/*
+ * Copyright © 2012 Keith Packard <keithp@keithp.com>
+ *
+ * This program is free software; you can redistribute it and/or modify
+ * it under the terms of the GNU General Public License as published by
+ * the Free Software Foundation; version 2 of the License.
+ *
+ * This program is distributed in the hope that it will be useful, but
+ * WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the GNU
+ * General Public License for more details.
+ *
+ * You should have received a copy of the GNU General Public License along
+ * with this program; if not, write to the Free Software Foundation, Inc.,
+ * 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA.
+ */
+
+package org.altusmetrum.AltosLib;
+
+public class AltosRecordTM extends AltosRecord {
+       public int      accel;
+       public int      pres;
+       public int      temp;
+       public int      batt;
+       public int      drogue;
+       public int      main;
+
+       public int      ground_accel;
+       public int      ground_pres;
+       public int      accel_plus_g;
+       public int      accel_minus_g;
+
+       public int      flight_accel;
+       public int      flight_vel;
+       public int      flight_pres;
+
+       /*
+        * Values for our MP3H6115A pressure sensor
+        *
+        * From the data sheet:
+        *
+        * Pressure range: 15-115 kPa
+        * Voltage at 115kPa: 2.82
+        * Output scale: 27mV/kPa
+        *
+        *
+        * 27 mV/kPa * 2047 / 3300 counts/mV = 16.75 counts/kPa
+        * 2.82V * 2047 / 3.3 counts/V = 1749 counts/115 kPa
+        */
+
+       static final double counts_per_kPa = 27 * 2047 / 3300;
+       static final double counts_at_101_3kPa = 1674.0;
+
+       static double
+       barometer_to_pressure(double count)
+       {
+               return ((count / 16.0) / 2047.0 + 0.095) / 0.009 * 1000.0;
+       }
+
+       public double raw_pressure() {
+               if (pres == MISSING)
+                       return MISSING;
+               return barometer_to_pressure(pres);
+       }
+
+       public double filtered_pressure() {
+               if (flight_pres == MISSING)
+                       return MISSING;
+               return barometer_to_pressure(flight_pres);
+       }
+
+       public double ground_pressure() {
+               if (ground_pres == MISSING)
+                       return MISSING;
+               return barometer_to_pressure(ground_pres);
+       }
+
+       public double battery_voltage() {
+               if (batt == MISSING)
+                       return MISSING;
+               return AltosConvert.cc_battery_to_voltage(batt);
+       }
+
+       public double main_voltage() {
+               if (main == MISSING)
+                       return MISSING;
+               return AltosConvert.cc_ignitor_to_voltage(main);
+       }
+
+       public double drogue_voltage() {
+               if (drogue == MISSING)
+                       return MISSING;
+               return AltosConvert.cc_ignitor_to_voltage(drogue);
+       }
+
+       /* Value for the CC1111 built-in temperature sensor
+        * Output voltage at 0°C = 0.755V
+        * Coefficient = 0.00247V/°C
+        * Reference voltage = 1.25V
+        *
+        * temp = ((value / 32767) * 1.25 - 0.755) / 0.00247
+        *      = (value - 19791.268) / 32768 * 1.25 / 0.00247
+        */
+
+       static double
+       thermometer_to_temperature(double thermo)
+       {
+               return (thermo - 19791.268) / 32728.0 * 1.25 / 0.00247;
+       }
+
+       public double temperature() {
+               if (temp == MISSING)
+                       return MISSING;
+               return thermometer_to_temperature(temp);
+       }
+
+       double accel_counts_per_mss() {
+               double  counts_per_g = Math.abs(accel_minus_g - accel_plus_g) / 2;
+
+               return counts_per_g / 9.80665;
+       }
+
+       public double acceleration() {
+               if (acceleration != MISSING)
+                       return acceleration;
+
+               if (ground_accel == MISSING || accel == MISSING)
+                       return MISSING;
+               return (ground_accel - accel) / accel_counts_per_mss();
+       }
+
+       public double accel_speed() {
+               if (speed != MISSING)
+                       return speed;
+               if (flight_vel == MISSING)
+                       return MISSING;
+               return flight_vel / (accel_counts_per_mss() * 100.0);
+       }
+
+       public void copy(AltosRecordTM old) {
+               super.copy(old);
+
+               version = old.version;
+               callsign = old.callsign;
+               serial = old.serial;
+               flight = old.flight;
+               rssi = old.rssi;
+               status = old.status;
+               state = old.state;
+               tick = old.tick;
+               accel = old.accel;
+               pres = old.pres;
+               temp = old.temp;
+               batt = old.batt;
+               drogue = old.drogue;
+               main = old.main;
+               flight_accel = old.flight_accel;
+               ground_accel = old.ground_accel;
+               flight_vel = old.flight_vel;
+               flight_pres = old.flight_pres;
+               ground_pres = old.ground_pres;
+               accel_plus_g = old.accel_plus_g;
+               accel_minus_g = old.accel_minus_g;
+       }
+
+       public AltosRecordTM clone() {
+               AltosRecordTM   n = (AltosRecordTM) super.clone();
+               n.copy(this);
+               return n;
+       }
+
+       void make_missing() {
+               accel = MISSING;
+               pres = MISSING;
+               temp = MISSING;
+               batt = MISSING;
+               drogue = MISSING;
+               main = MISSING;
+
+               flight_accel = 0;
+               flight_vel = 0;
+               flight_pres = 0;
+
+               ground_accel = 0;
+               ground_pres = 0;
+               accel_plus_g = 0;
+               accel_minus_g = 0;
+       }
+
+       public AltosRecordTM(AltosRecord old) {
+               super.copy(old);
+               make_missing();
+       }
+
+       public AltosRecordTM() {
+               super();
+               make_missing();
+       }
+}