Mercurial > public > ostc4
view Discovery/Src/unit.c @ 901:e4e9acfde839 Evo_2_23
Bugfix simulator/planer:
For deco calculation two structures are used. The calculation structure and the input structure. During simulation fast forward (+5min) the input structure is manipulated. Especially for vpm calculation it could happen that the input structure was manipulated and then overwritten by the calculation structure => deco and tts may have wrong values. To avoid this thedeco calculation status is now checked before doing the FF manupulation. Based an calculation state deco or input structures are manipulated.
Surface time stamp in planer view:
The planer used its own (buggy) implementation for calculation of tts. The timestamp for the surface arrival did not match the bottom time + TTS. The new implementation uses the tts calculated by the deco loop for generation of surface time stamp.
author | Ideenmodellierer |
---|---|
date | Wed, 02 Oct 2024 22:07:13 +0200 |
parents | 269e57ac4e56 |
children |
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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 'f'; else return 'm'; } char unit_depth_char2_T105(void) { if(settingsGetPointer()->nonMetricalSystem) return 't'; 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; } } int16_t unit_temperature_integer(int16_t input_celsius) { if(settingsGetPointer()->nonMetricalSystem == 0) return input_celsius; else { return ((input_celsius * 9 / 5) + 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; } }