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/*
* Copyright © 2010 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 abstract class AltosRecord implements Comparable <AltosRecord>, Cloneable {
public static final int seen_flight = 1;
public static final int seen_sensor = 2;
public static final int seen_temp_volt = 4;
public static final int seen_deploy = 8;
public static final int seen_gps_time = 16;
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 final static int MISSING = 0x7fffffff;
/* Every AltosRecord implementation provides these fields */
public int version;
public String callsign;
public int serial;
public int flight;
public int rssi;
public int status;
public int state;
public int tick;
public AltosGPS gps;
public boolean new_gps;
public double time; /* seconds since boost */
public int device_type;
public int config_major;
public int config_minor;
public int apogee_delay;
public int main_deploy;
public int flight_log_max;
public String firmware_version;
public AltosRecordCompanion companion;
/* Telemetry sources have these values recorded from the flight computer */
public double kalman_height;
public double kalman_speed;
public double kalman_acceleration;
/*
* Abstract methods that convert record data
* to standard units:
*
* pressure: Pa
* voltage: V
* acceleration: m/s²
* speed: m/s
* height: m
* temperature: °C
*/
abstract public double pressure();
abstract public double ground_pressure();
abstract public double acceleration();
public double altitude() {
double p = pressure();
if (p == MISSING)
return MISSING;
return AltosConvert.pressure_to_altitude(p);
}
public double ground_altitude() {
double p = ground_pressure();
if (p == MISSING)
return MISSING;
return AltosConvert.pressure_to_altitude(p);
}
public double height() {
double g = ground_altitude();
double a = altitude();
if (g == MISSING)
return MISSING;
if (a == MISSING)
return MISSING;
return a - g;
}
public double battery_voltage() { return MISSING; }
public double main_voltage() { return MISSING; }
public double drogue_voltage() { return MISSING; }
public double temperature() { return MISSING; }
public AltosIMU imu() { return null; }
public AltosMag mag() { return null; }
public String state() {
return AltosLib.state_name(state);
}
public int compareTo(AltosRecord o) {
return tick - o.tick;
}
abstract public AltosRecord clone();
public void copy(AltosRecord old) {
seen = old.seen;
version = old.version;
callsign = old.callsign;
serial = old.serial;
flight = old.flight;
rssi = old.rssi;
status = old.status;
state = old.state;
tick = old.tick;
gps = new AltosGPS(old.gps);
new_gps = old.new_gps;
companion = old.companion;
kalman_acceleration = old.kalman_acceleration;
kalman_speed = old.kalman_speed;
kalman_height = old.kalman_height;
}
public AltosRecord() {
seen = 0;
version = 0;
callsign = "N0CALL";
serial = 0;
flight = 0;
rssi = 0;
status = 0;
state = AltosLib.ao_flight_startup;
tick = 0;
gps = new AltosGPS();
new_gps = false;
companion = null;
kalman_acceleration = MISSING;
kalman_speed = MISSING;
kalman_height = MISSING;
}
}
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