kopia lustrzana https://github.com/pjalocha/esp32-ogn-tracker
64 wiersze
2.8 KiB
C++
64 wiersze
2.8 KiB
C++
#ifndef __ATMOSPHERE_H__
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#define __ATMOSPHERE_H__
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#include <math.h>
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#include <stdint.h>
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class Atmosphere
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{ public:
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// int32_t Pressure; // [ Pa ]
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// int32_t Altitude; // [0.1 m ]
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// int32_t Temperature; // [0.1 degC]
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// altitude vs. pressure // 20000, 30000, 40000, 50000, 60000, 70000, 80000, 90000, 100000, 110000 // [ Pa]
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static const int32_t StdAltTable[10]; // = { 117764, 91652, 71864, 55752, 42070, 30126, 19493, 9886, 1109, -6984 } ; // [0.1 m]
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public:
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// dH/dP = -R/g*T => R = 287.04m^2/K/sec^2, g = 9.80655m/s^2
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static int32_t PressureLapseRate(int32_t Pressure, int32_t Temperature=150) // [Pa], [0.1 degC] => [0.0001 m/Pa]
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{ return -((int32_t)29270*(Temperature+2732)+Pressure/2)/Pressure; }
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// int32_t PressureLapseRate(void) { return PressureLapseRate(Pressure, Temperature); }
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static const int32_t StdPressureAtSeaLevel = 101325; // [Pa]
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static const int32_t StdPressureAt11km = 22632; // [Pa]
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static const int32_t StdPressureAt20km = 5475; // [Pa]
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static const int32_t StdTemperatureLapseRate = -65; // [0.1 degC/1000m] valid till 11km
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static const int32_t StdTemperatureAtSeaLevel = 150; // [0.1 degC ]
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static const int32_t StdTemperatureAt11km = -565; // [0.1 degC ]
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static int32_t StdTemperature(int32_t Altitude) // [0.1 m ] valid till 20km
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{ if(Altitude>110000) return StdTemperatureAt11km;
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return StdTemperatureAtSeaLevel+(StdTemperatureLapseRate*Altitude-5000)/10000; }
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static int32_t AltitudeDelta(int32_t PressureDelta, int32_t PressureLapseRate) // [Pa], [0.0001 m/Pa]
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{ return (PressureDelta*PressureLapseRate)/100; } // [0.01m]
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static int32_t AltitudeDelta(int32_t PressureDelta, int32_t Pressure, int32_t Temperature) // [Pa], [Pa], [0.1degC]
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{ int32_t PLR=PressureLapseRate(Pressure, Temperature); return AltitudeDelta(PressureDelta, PLR); } // [0.01m]
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static int32_t StdAltitude(int32_t Pressure, int32_t PressStep=100) // [Pa]
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{ int32_t Idx=(Pressure+5000)/10000; Idx-=2;
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if(Idx<0) Idx=0; else if(Idx>9) Idx=9;
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int32_t Press = 10000*(Idx+2);
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int32_t Altitude = 10*StdAltTable[Idx];
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for( ; ; )
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{ int32_t Temp=StdTemperature(Altitude/10);
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int32_t Delta=Pressure-Press; if(Delta==0) break;
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if(Delta>PressStep) Delta=PressStep;
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else if(Delta<(-PressStep)) Delta=(-PressStep);
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Altitude+=AltitudeDelta(Delta, Press, Temp);
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Press+=Delta;
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}
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return Altitude/10; } // [0.1m]
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#ifdef NO_RTOS
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static int32_t StdAltitude_float(int32_t Pressure)
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{ return floor(443300*(1-powf((float)Pressure/(float)101325.0, (float)0.190295))+0.5); }
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#endif
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} ;
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#endif // __ATMOSPHERE_H__
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