Version modifié Polytech Paris Sud correction erreur de calcul sur la lib initiale
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MS5607Base.h
00001 /* 00002 Copyright (c) 2012, Senio Networks, Inc. 00003 00004 Permission is hereby granted, free of charge, to any person obtaining a copy 00005 of this software and associated documentation files (the "Software"), to deal 00006 in the Software without restriction, including without limitation the rights 00007 to use, copy, modify, merge, publish, distribute, sublicense, and/or sell 00008 copies of the Software, and to permit persons to whom the Software is 00009 furnished to do so, subject to the following conditions: 00010 00011 The above copyright notice and this permission notice shall be included in 00012 all copies or substantial portions of the Software. 00013 00014 THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND, EXPRESS OR 00015 IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF MERCHANTABILITY, 00016 FITNESS FOR A PARTICULAR PURPOSE AND NONINFRINGEMENT. IN NO EVENT SHALL THE 00017 AUTHORS OR COPYRIGHT HOLDERS BE LIABLE FOR ANY CLAIM, DAMAGES OR OTHER 00018 LIABILITY, WHETHER IN AN ACTION OF CONTRACT, TORT OR OTHERWISE, ARISING FROM, 00019 OUT OF OR IN CONNECTION WITH THE SOFTWARE OR THE USE OR OTHER DEALINGS IN 00020 THE SOFTWARE. 00021 */ 00022 00023 #ifndef MS5607_BASE_H 00024 #define MS5607_BASE_H 00025 00026 class MS5607Base { 00027 public: 00028 void init(float itemp=0,float ipress=0) { 00029 writeCommand(RESET, 3); 00030 c1 = readPROM(1); 00031 c2 = readPROM(2); 00032 c3 = readPROM(3); 00033 c4 = readPROM(4); 00034 c5 = readPROM(5); 00035 c6 = readPROM(6); 00036 inittemp = itemp; 00037 initpress= ipress; 00038 } 00039 00040 void printCoefficients() { 00041 printf("%d, %d, %d, %d, %d, %d\n", c1, c2, c3, c4, c5, c6); 00042 } 00043 00044 int getRawTemperature() { 00045 return readADC(ADC_D2 | OSR_4096); 00046 } 00047 00048 int getRawPressure() { 00049 return readADC(ADC_D1 | OSR_4096); 00050 } 00051 00052 float getTemperature() { 00053 int dT = getRawTemperature() - ((0x0FFFF&c5) << 8); 00054 int temp = 2000 + (((int64_t)dT * (0x0FFFF&c6)) >> 23); 00055 00056 // 2nd order temperature compensation 00057 if (temp < 2000) { 00058 int t2 = ((int64_t) dT * dT )>> 31; 00059 temp -= t2; 00060 } 00061 00062 return float(temp) / 100; 00063 } 00064 00065 float getPressure() { 00066 int dT = getRawTemperature() - (c5 << 8); 00067 int temp = 2000 + ((dT * c6) >> 23); 00068 int64_t off = ((int64_t) c2 << 17) + ((int64_t) dT * c4 >> 6); 00069 int64_t sens = ((int64_t) c1 << 16) + ((int64_t) dT * c3 >> 7); 00070 00071 // 2nd order temperature compensation 00072 if (temp < 2000) { 00073 int64_t off2 = (int64_t) 61 * (temp - 2000) * (temp - 2000) >> 4; 00074 int64_t sens2 = (int64_t) 2 * (temp - 2000) * (temp - 2000); 00075 if (temp < -1500) { 00076 off2 += (int64_t) 15 * (temp + 1500) * (temp + 1500); 00077 sens2 += (int64_t) 8 * (temp + 1500) * (temp + 1500); 00078 } 00079 off -= off2; 00080 sens -= sens2; 00081 } 00082 00083 return float((((int64_t) getRawPressure() * sens >> 21) - off) >> 15); 00084 } 00085 00086 float getAltitude(int presssure = 0) { 00087 return toAltitude(presssure ? presssure : (int) getPressure()); 00088 } 00089 00090 protected: 00091 int32_t c1, c2, c3, c4, c5, c6; 00092 float inittemp, initpress; 00093 enum { 00094 RESET = 0x1E, 00095 ADC_READ = 0x00, 00096 ADC_CONV = 0x40, 00097 ADC_D1 = 0x00, 00098 ADC_D2 = 0x10, 00099 OSR_256 = 0x00, 00100 OSR_512 = 0x02, 00101 OSR_1024 = 0x04, 00102 OSR_2048 = 0x06, 00103 OSR_4096 = 0x08, 00104 PROM_READ = 0xA0 00105 }; 00106 00107 virtual void writeCommand(int command, int ms = 0) = 0; 00108 virtual int readPROM(int address) = 0; 00109 virtual int readADC(int command) = 0; 00110 00111 00112 00113 float toAltitude(int pressure) { 00114 // Ref. 29124-AltimeterAppNote1.pdf 00115 const float R = 287.052; // specific gas constant R*/M0 00116 const float g = 9.80665; // standard gravity 00117 const float t_grad = 0.0065; // gradient of temperature 00118 if(inittemp==0) inittemp=15; 00119 if(initpress==0) initpress=101325; 00120 float t0 = 273.15 + inittemp; // temperature at 0 altitude 00121 float p0 = initpress;// 101700; // pressure at 0 altitude 00122 00123 return t0 / t_grad * (1 - exp((t_grad * R / g) * log(pressure / p0))); 00124 } 00125 }; 00126 00127 #endif
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