test
Dependencies: mbed Lab5-03_create_satcode_step6_lite HEPTA_CDH_lite HEPTA_COM_lite LPS25HB_I2C HEPTA_SENSOR_lite HEPTA_EPS_lite
Diff: main.cpp
- Revision:
- 4:a4ea741ca530
- Parent:
- 3:e5ae22e02335
--- a/main.cpp Tue Aug 17 11:07:04 2021 +0000 +++ b/main.cpp Sat Aug 20 11:38:09 2022 +0000 @@ -3,103 +3,131 @@ #include "HEPTA_CDH.h" #include "HEPTA_SENSOR.h" #include "HEPTA_COM.h" +#include "LPS.h" HEPTA_CDH cdh(PB_5, PB_4, PB_3, PA_8, "sd"); HEPTA_EPS eps(PA_0,PA_4); HEPTA_SENSOR sensor(PA_7,PB_7,PB_6,0xD0); HEPTA_COM com(PA_9,PA_10,9600); DigitalOut condition(PB_1); -Serial sat(USBTX,USBRX, 38400); +DigitalOut analog_switch(PA_3); +Serial sat(USBTX,USBRX, 9600); +//I2C i2c(PB_7, PB_6); +I2C i2c(D4,D5); Timer sattime; + +LPS ps(i2c); +DigitalOut sp1(PA_1); +Ticker press; +Ticker sound; +int flag = 0; //condition flag +float batvol, temp; //voltage, temperature +int rcmd=0,cmdflag=0; //command variable +int i, ct = 0; +float pressure = 0.0, altitude = 0.0, temperature = 0.0; +float ax,ay,az,gx,gy,gz; +char cmd1,cmd2,cmd3; +int oto = 0; +#define mC 261.626 +#define mD 293.665 +#define mE 329.628 +#define mF 349.228 +#define mG 391.995 +#define mA 440.000 +#define mB 493.883 +float mm[]={mC*4,mD*4,mE*4,mF*4,mG*4,mA*4,mB*4,mC*8}; //timbre + +void tick(void) +{ + sp1.write(oto); + oto=!oto; +} + +void pre() { + com.printf("HEPTASAT::Time = %.4f [s], batvol = %.4f [V], temp = %.4f [deg C], altitude = %.4f [m]\r\n",sattime.read(),batvol,temp,altitude); + com.printf(" ::ax = %.4f, ay = %.4f, az = %.4f, gx = %.4f, gy = %.4f, gz = %.4f\r\n",ax,ay,az,gx,gy,gz); + +} + int main() { sat.printf("From Sat : Nominal Operation\r\n"); com.printf("From Sat : Nominal Operation\r\n"); - int flag = 0; //condition flag - float batvol, temp; //voltage, temperature - int rcmd=0,cmdflag=0; //command variable sattime.start(); - eps.turn_on_regulator();//turn on 3.3V conveter - for(int i=0;i<50;i++){ + eps.turn_on_regulator(); //turn on 3.3V conveter + analog_switch = 1; //turn on analog switch (transceiver mode) + + mkdir("/sd/mydir", 0777); + FILE *fp = fopen("/sd/mydir/sdtest.csv", "w"); + if(fp == NULL) { + error("Could not open file for write\r\n"); + } + fclose(fp); + + // initialize the pressure sensor + if (!ps.init()){ + printf("Failed to autodetect pressure sensor!\r\n"); + while (1); + } + ps.enableDefault(); // setting the pressure sensor + while(1){ com.xbee_receive(&rcmd,&cmdflag); - - //satellite condition led - condition = !condition; - - //senssing HK data - eps.vol(&batvol); - sensor.temp_sense(&temp); - - //Transmitting HK data to Ground Station(GS) - com.printf("HEPTASAT::Condition = %d, Time = %f [s], batvol = %2f [V], temp = %2f [deg C]\r\n",flag,sattime.read(),batvol,temp); - wait_ms(1000); - - //Power Saving Mode - if((batvol <= 3.5) | (temp > 35.0)){ - eps.shut_down_regulator(); - com.printf("Power saving mode ON\r\n"); - flag = 1; - } else if((flag == 1) & (batvol > 3.7) & (temp <= 25.0)) { - eps.turn_on_regulator(); - com.printf("Power saving mode OFF\r\n"); - flag = 0; - } - if(cmdflag == 1){ - if(rcmd == 'a'){ - sat.printf("rcmd=%c,cmdflag=%d\r\n",rcmd,cmdflag); - com.printf("Hepta-Sat Lite Uplink Ok\r\n"); - for(int j=0;j<5;j++){ - com.printf("Hello World!\r\n"); - condition = 1; - wait_ms(1000); + if(rcmd == 'm'){ + com.initialize(); //initializing + FILE *fp = fopen("/sd/mydir/sdtest.csv", "a"); + int count = 0; + press.attach(&pre, 1.0); + while(1){ + com.xbee_receive(&rcmd,&cmdflag); + //satellite condition led + condition = !condition; + //sensing HK data + eps.vol(&batvol); + sensor.temp_sense(&temp); + + //sensing the + sensor.sen_acc(&ax,&ay,&az); + sensor.sen_gyro(&gx,&gy,&gz); + pressure = ps.readPressureMillibars(); + altitude = ps.pressureToAltitudeMeters(pressure); + temperature = ps.readTemperatureC(); + //if((count % 10) == 0){ +// com.printf("HEPTASAT::Time = %.4f [s], batvol = %.4f [V], temp = %.4f [deg C], altitude = %.4f [m]\r\n",sattime.read(),batvol,temp,altitude); +// com.printf(" ::ax = %.4f, ay = %.4f, az = %.4f, gx = %.4f, gy = %.4f, gz = %.4f\r\n",ax,ay,az,gx,gy,gz); +// } + fprintf(fp,"%f, %f, %f, %f, %f, %f, %f, %f, %f, %f\r\n",sattime.read(),batvol,temp,altitude,ax,ay,az,gx,gy,gz); + wait_ms(100); + if(rcmd == 'f'){ + fclose(fp); + press.detach(); + sat.printf("finish sensing\r\n"); + com.printf("finish sensing\r\n"); + break; + } + count++; } - }else if(rcmd == 'b') { - sat.printf("rcmd=%c,cmdflag=%d\r\n",rcmd,cmdflag); - com.printf("Hepta-Sat Lite Uplink Ok\r\n"); - char str[100]; - mkdir("/sd/mydir", 0777); - FILE *fp = fopen("/sd/mydir/satdata.txt","w"); - if(fp == NULL) { - error("Could not open file for write\r\n"); - } - for(int i = 0; i < 10; i++) { - eps.vol(&batvol); - fprintf(fp,"%f\r\n",batvol); - condition = 1; - wait_ms(1000); - } - fclose(fp); - fp = fopen("/sd/mydir/satdata.txt","r"); - for(int i = 0; i < 10; i++) { - fgets(str,100,fp); - com.puts(str); + } + } + if(rcmd == 'e'){ + sat.printf("From Sat : End of while\r\n"); + com.printf("From Sat : End of while\r\n"); + com.initialize(); //initializing + while(1){ + com.xbee_receive(&rcmd,&cmdflag); + if(rcmd == 'z'){ + oto = 0; + break; } - fclose(fp); - }else if(rcmd == 'c'){ - sat.printf("rcmd=%c,cmdflag=%d\r\n",rcmd,cmdflag); - com.printf("Hepta-Sat Lite Uplink Ok\r\n"); - float ax,ay,az; - for(int i = 0; i < 10; i++) { - sensor.sen_acc(&ax,&ay,&az); - com.printf("%f,%f,%f\r\n",ax,ay,az); - wait_ms(1000); + for(i=0;i < sizeof(mm)/sizeof(mm[0]);i++) { + sound.attach(&tick,1.0/mm[i]/2.0); //If warning appear, ignore + wait(0.5f); } - }else if(rcmd == 'd'){ - sat.printf("rcmd=%c,cmdflag=%d\r\n",rcmd,cmdflag); - com.printf("Hepta-Sat Lite Uplink Ok\r\n"); - float gx,gy,gz; - for(int i = 0; i < 10; i++) { - sensor.sen_gyro(&gx,&gy,&gz); - com.printf("%f,%f,%f\r\n",gx,gy,gz); - wait_ms(1000); - } - }else if(rcmd == 'e'){ - - - + sound.detach(); + i = 0; } - com.initialize(); //initializing + break; } + com.initialize(); //initializing } sattime.stop(); sat.printf("From Sat : End of operation\r\n");