Library to work with the MS5611 pressure sensors. Forked from the MS5607 library
Dependents: MS5611Example Atlas HC-06_MPU9250_F303K_Stream
Fork of MS5607 by
MS5611Base.h
- Committer:
- matgyver
- Date:
- 2014-06-24
- Revision:
- 1:847720b736ea
File content as of revision 1:847720b736ea:
/* Copyright (c) 2012, Senio Networks, Inc. Permission is hereby granted, free of charge, to any person obtaining a copy of this software and associated documentation files (the "Software"), to deal in the Software without restriction, including without limitation the rights to use, copy, modify, merge, publish, distribute, sublicense, and/or sell copies of the Software, and to permit persons to whom the Software is furnished to do so, subject to the following conditions: The above copyright notice and this permission notice shall be included in all copies or substantial portions of the Software. THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND, EXPRESS OR IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF MERCHANTABILITY, FITNESS FOR A PARTICULAR PURPOSE AND NONINFRINGEMENT. IN NO EVENT SHALL THE AUTHORS OR COPYRIGHT HOLDERS BE LIABLE FOR ANY CLAIM, DAMAGES OR OTHER LIABILITY, WHETHER IN AN ACTION OF CONTRACT, TORT OR OTHERWISE, ARISING FROM, OUT OF OR IN CONNECTION WITH THE SOFTWARE OR THE USE OR OTHER DEALINGS IN THE SOFTWARE. */ /* MS5611 Modifications Aerodyne Labs Matthew Nelson - 2014 This library was originally the MS5607 library. It has been modified to to be used the MS5611 Pressure sensor */ #ifndef MS5611_BASE_H #define MS5611_BASE_H class MS5611Base { public: void printCoefficients() { printf("%d, %d, %d, %d, %d, %d \r\n", c1, c2, c3, c4, c5, c6); } int getRawTemperature() { return readADC(ADC_D2 | OSR_4096); } int getRawPressure() { return readADC(ADC_D1 | OSR_4096); } float getTemperature() { int dT = getRawTemperature() - (c5 << 8); int temp = 2000 + ((dT * c6) >> 23); // 2nd order temperature compensation if (temp < 2000) { int t2 = (int64_t) dT * dT >> 31; temp -= t2; } return float(temp) / 100; } float getPressure() { int dT = getRawTemperature() - (c5 << 8); int temp = 2000 + ((dT * c6) >> 23); int64_t off = ((int64_t) c2 << 16) + ((int64_t) dT * c4 >> 7); int64_t sens = ((int64_t) c1 << 15) + ((int64_t) dT * c3 >> 8); // 2nd order temperature compensation if (temp < 2000) { int64_t off2 = (int64_t) 5 * (temp - 2000) * (temp - 2000) >> 1; int64_t sens2 = (int64_t) 5 * (temp - 2000) * (temp - 2000) >> 2; if (temp < -1500) { off2 += (int64_t) 7 * (temp + 1500) * (temp + 1500); sens2 += (int64_t) 11 * (temp + 1500) * (temp + 1500) >> 1; } off -= off2; sens -= sens2; } return float((((int64_t) getRawPressure() * sens >> 21) - off) >> 15); } float getAltitude(int presssure = 0) { return toAltitude(presssure ? presssure : (int) getPressure()); } protected: int32_t c1, c2, c3, c4, c5, c6; enum { RESET = 0x1E, ADC_READ = 0x00, ADC_CONV = 0x40, ADC_D1 = 0x00, ADC_D2 = 0x10, OSR_256 = 0x00, OSR_512 = 0x02, OSR_1024 = 0x04, OSR_2048 = 0x06, OSR_4096 = 0x08, PROM_READ = 0xA0 }; virtual void writeCommand(int command, int ms = 0) = 0; virtual int readPROM(int address) = 0; virtual int readADC(int command) = 0; void init() { writeCommand(RESET, 3); c1 = readPROM(1); c2 = readPROM(2); c3 = readPROM(3); c4 = readPROM(4); c5 = readPROM(5); c6 = readPROM(6); } float toAltitude(int pressure) { // Ref. 29124-AltimeterAppNote1.pdf const float R = 287.052; // specific gas constant R*/M0 const float g = 9.80665; // standard gravity const float t_grad = 0.0065; // gradient of temperature const float t0 = 273.15 + 15; // temperature at 0 altitude const float p0 = 101325; // pressure at 0 altitude return t0 / t_grad * (1 - exp((t_grad * R / g) * log(pressure / p0))); } }; #endif