Mercurial > public > ostc4
view Discovery/Src/unit.c @ 222:9b4b3decd9ba div-fixes-3
Bugfix: correct presentation error in tissues custom view
The green vertical line in the N2/He bars show the inspired partial
pressures of the respective gasses. Obviously, the tissue partial
pressure is always lower on an initial descent, than the inspired partial
pressure of the respective gas. Further, when for a given depth, the
inspired partial pressure is equal to the tissue partial
pressure, the tissue gets fully saturated, so the bars stop at
the green line.
For N2, a simple presentation error was present. As the body is always
saturated with about 75% of N2 (according to the Buelmann algorithm),
the tissue N2 was shifted left for that amount, but the inspired N2 line
was not. So, the N2 green vertical line was too far to the right. Corrected
this.
Signed-off-by: Jan Mulder <jlmulder@xs4all.nl>
author | Jan Mulder <jlmulder@xs4all.nl> |
---|---|
date | Fri, 29 Mar 2019 14:00:43 +0100 |
parents | 5f11787b4f42 |
children | 1c95f811967c |
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/////////////////////////////////////////////////////////////////////////////// /// -*- coding: UTF-8 -*- /// /// \file Discovery/Src/unit.c /// \brief input to meter/celsius or feet/farenheit /// \author heinrichs weikamp gmbh /// \date 24-Feb-2015 /// /// \details /// /// $Id$ /////////////////////////////////////////////////////////////////////////////// /// \par Copyright (c) 2014-2018 Heinrichs Weikamp gmbh /// /// 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, either version 3 of the License, or /// (at your option) any later version. /// /// 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, see <http://www.gnu.org/licenses/>. ////////////////////////////////////////////////////////////////////////////// /* Includes ------------------------------------------------------------------*/ #include "unit.h" #include "settings.h" /* Exported variables --------------------------------------------------------*/ /* Private types -------------------------------------------------------------*/ uint8_t test; /* Private variables ---------------------------------------------------------*/ /* Private variables with external access via get_xxx() function -------------*/ /* Private function prototypes -----------------------------------------------*/ /* Announced function prototypes -----------------------------------------------*/ /* Exported functions --------------------------------------------------------*/ char unit_depth_char1_T105(void) { if(settingsGetPointer()->nonMetricalSystem) return '\''; else return 'm'; } char unit_depth_char2_T105(void) { if(settingsGetPointer()->nonMetricalSystem) return ' '; else return '\004'; // 004 is nop } char unit_depth_char1(void) { if(settingsGetPointer()->nonMetricalSystem) return 'f'; else return 'm'; } char unit_depth_char2(void) { if(settingsGetPointer()->nonMetricalSystem) return 't'; else return '\004'; // 004 is nop } float unit_depth_float(float input_meter) { if(settingsGetPointer()->nonMetricalSystem == 0) return input_meter; else { return 3.2808f * input_meter; } } uint16_t unit_depth_integer(uint16_t input_meter) { if(settingsGetPointer()->nonMetricalSystem == 0) return input_meter; else { return (input_meter * 10) / 3; } } float unit_temperature_float(float input_celsius) { if(settingsGetPointer()->nonMetricalSystem == 0) return input_celsius; else { return input_celsius * (9.0f/5.0f) + 32; } } uint16_t unit_speed_integer(uint16_t input_meterPerMinute) { if(settingsGetPointer()->nonMetricalSystem == 0) return input_meterPerMinute; else { return (input_meterPerMinute * 10) / 3; } } /* Quelle: https://de.wikipedia.org/wiki/Luftdruck */ /* const float luftdruckStartMinus300[15] = { 1.0530f, 1.0396f, 1.0263f, 1.01325f, // 0 m 1.0003f, 0.9876f, 0.9750f, 0.9625f, 0.9503f, 0.9381f, 0.9262f, 0.9144f, 0.9027f, 0.8912f, // 1000 m 0.8358f }; */ const int luftdruckStartMinus300[15] = { 1053, 1040, 1026, 1013, // 0 m 1000, 988, 975, 962, 950, 938, 926, 914, 903, 891, // 1000 m 836 }; int unit_SeaLevelRelation_integer(int input_atmospheric_mbar) { int i = 0; int distance1, distance2; for(i=0;i<15;i++) { if(input_atmospheric_mbar >= luftdruckStartMinus300[i]) break; } if(i >= 14) return 1500; else if(i == 0) return -300; else { distance1 = input_atmospheric_mbar - luftdruckStartMinus300[i]; distance2 = luftdruckStartMinus300[i-1] - input_atmospheric_mbar; if(distance2 < distance1) i -= 1; return (i*100) - 300; } }