test
Dependencies: mbed Lab5-03_create_satcode_step6_lite HEPTA_CDH_lite HEPTA_COM_lite LPS25HB_I2C HEPTA_SENSOR_lite HEPTA_EPS_lite
main.cpp
- Committer:
- heptasat2021
- Date:
- 2021-08-17
- Revision:
- 3:e5ae22e02335
- Parent:
- 2:30f72f09756e
- Child:
- 4:a4ea741ca530
File content as of revision 3:e5ae22e02335:
#include "mbed.h" #include "HEPTA_EPS.h" #include "HEPTA_CDH.h" #include "HEPTA_SENSOR.h" #include "HEPTA_COM.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); Timer sattime; 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++){ 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); } }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); } 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); } }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'){ } com.initialize(); //initializing } } sattime.stop(); sat.printf("From Sat : End of operation\r\n"); com.printf("From Sat : End of operation\r\n"); }