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Diffstat (limited to 'altoslib/AltosRecordTM.java')
-rw-r--r-- | altoslib/AltosRecordTM.java | 199 |
1 files changed, 199 insertions, 0 deletions
diff --git a/altoslib/AltosRecordTM.java b/altoslib/AltosRecordTM.java new file mode 100644 index 00000000..afb70790 --- /dev/null +++ b/altoslib/AltosRecordTM.java @@ -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(); + } +} |