altosui: Support MM telemetry packets
[fw/altos] / altoslib / AltosRecord.java
index 10ef30613d32a31c037e1d8c9974b58e9d761fbb..e468f84b425b705a1b6a498d309679c11449b18d 100644 (file)
@@ -22,8 +22,7 @@ import java.text.*;
 import java.util.HashMap;
 import java.io.*;
 
-public class AltosRecord implements Comparable <AltosRecord> {
-       public final static int MISSING = 0x7fffffff;
+public class AltosRecord implements Comparable <AltosRecord>, Cloneable {
 
        public static final int seen_flight = 1;
        public static final int seen_sensor = 2;
@@ -33,8 +32,13 @@ public class AltosRecord implements Comparable <AltosRecord> {
        public static final int seen_gps_lat = 32;
        public static final int seen_gps_lon = 64;
        public static final int seen_companion = 128;
-       public int                      seen;
 
+       public int      seen;
+       
+       public final static int MISSING = 0x7fffffff;
+
+       /* Every AltosRecord implementation provides these fields */
+       
        public int      version;
        public String   callsign;
        public int      serial;
@@ -44,31 +48,13 @@ public class AltosRecord implements Comparable <AltosRecord> {
        public int      state;
        public int      tick;
 
-       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 double   acceleration;
-       public double   speed;
-       public double   height;
-
-       public int      flight_accel;
-       public int      flight_vel;
-       public int      flight_pres;
+       /* Current flight dynamic state */
+       public double   acceleration;   /* m/s² */
+       public double   speed;          /* m/s */
+       public double   height;         /* m */
 
        public AltosGPS gps;
-       public boolean          new_gps;
-
-       public AltosIMU imu;
-       public AltosMag mag;
+       public boolean  new_gps;
 
        public double   time;   /* seconds since boost */
 
@@ -83,45 +69,42 @@ public class AltosRecord implements Comparable <AltosRecord> {
        public AltosRecordCompanion companion;
 
        /*
-        * Values for our MP3H6115A pressure sensor
-        *
-        * From the data sheet:
+        * Abstract methods that convert record data
+        * to standard units:
         *
-        * 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
+        *      pressure:       Pa
+        *      voltage:        V
+        *      acceleration:   m/s²
+        *      speed:          m/s
+        *      height:         m
+        *      temperature:    °C
         */
 
-       public static final double counts_per_kPa = 27 * 2047 / 3300;
-       public static final double counts_at_101_3kPa = 1674.0;
+       public double raw_pressure() { return MISSING; }
 
-       public static double
-       barometer_to_pressure(double count)
-       {
-               return ((count / 16.0) / 2047.0 + 0.095) / 0.009 * 1000.0;
-       }
+       public double filtered_pressure() { return MISSING; }
 
-       public double raw_pressure() {
-               if (pres == MISSING)
-                       return MISSING;
-               return barometer_to_pressure(pres);
-       }
+       public double ground_pressure() { return MISSING; }
 
-       public double filtered_pressure() {
-               if (flight_pres == MISSING)
-                       return MISSING;
-               return barometer_to_pressure(flight_pres);
-       }
+       public double battery_voltage() { return MISSING; }
 
-       public double ground_pressure() {
-               if (ground_pres == MISSING)
-                       return MISSING;
-               return barometer_to_pressure(ground_pres);
-       }
+       public double main_voltage() { return MISSING; }
+
+       public double drogue_voltage() { return MISSING; }
+
+       public double temperature() { return MISSING; }
+       
+       public double acceleration() { return MISSING; }
+
+       public double accel_speed() { return MISSING; }
+
+       public AltosIMU imu() { return null; }
+
+       public AltosMag mag() { return null; }
+
+       /*
+        * Convert various pressure values to altitude
+        */
 
        public double raw_altitude() {
                double p = raw_pressure();
@@ -138,8 +121,9 @@ public class AltosRecord implements Comparable <AltosRecord> {
        }
 
        public double filtered_altitude() {
-               if (height != MISSING && ground_pres != MISSING)
-                       return height + ground_altitude();
+               double  ga = ground_altitude();
+               if (height != MISSING && ga != MISSING)
+                       return height + ga;
 
                double  p = filtered_pressure();
                if (p == MISSING)
@@ -167,94 +151,17 @@ public class AltosRecord implements Comparable <AltosRecord> {
                return r - g;
        }
 
-       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
-        */
-
-       public 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);
-       }
-
-       public 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 String state() {
                return AltosLib.state_name(state);
        }
 
-       public static String gets(FileInputStream s) throws IOException {
-               int c;
-               String  line = "";
-
-               while ((c = s.read()) != -1) {
-                       if (c == '\r')
-                               continue;
-                       if (c == '\n') {
-                               return line;
-                       }
-                       line = line + (char) c;
-               }
-               return null;
-       }
-
        public int compareTo(AltosRecord o) {
                return tick - o.tick;
        }
 
-       public AltosRecord(AltosRecord old) {
-               version = old.version;
+       public void copy(AltosRecord old) {
                seen = old.seen;
+               version = old.version;
                callsign = old.callsign;
                serial = old.serial;
                flight = old.flight;
@@ -262,32 +169,27 @@ public class AltosRecord implements Comparable <AltosRecord> {
                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;
                acceleration = old.acceleration;
                speed = old.speed;
                height = old.height;
                gps = new AltosGPS(old.gps);
                new_gps = false;
                companion = old.companion;
-               imu = old.imu;
-               mag = old.mag;
+       }
+
+       public AltosRecord clone() {
+               try {
+                       AltosRecord n = (AltosRecord) super.clone();
+                       n.copy(this);
+                       return n;
+               } catch (CloneNotSupportedException e) {
+                       return null;
+               }
        }
 
        public AltosRecord() {
-               version = 0;
                seen = 0;
+               version = 0;
                callsign = "N0CALL";
                serial = 0;
                flight = 0;
@@ -295,19 +197,6 @@ public class AltosRecord implements Comparable <AltosRecord> {
                status = 0;
                state = AltosLib.ao_flight_startup;
                tick = 0;
-               accel = MISSING;
-               pres = MISSING;
-               temp = MISSING;
-               batt = MISSING;
-               drogue = MISSING;
-               main = MISSING;
-               flight_accel = 0;
-               ground_accel = 0;
-               flight_vel = 0;
-               flight_pres = 0;
-               ground_pres = 0;
-               accel_plus_g = 0;
-               accel_minus_g = 0;
                acceleration = MISSING;
                speed = MISSING;
                height = MISSING;