I2C BAE standalone hardware testing
Dependencies: FreescaleIAP mbed-rtos mbed
Fork of ACS_Flowchart_BAE_1 by
Diff: ACS.cpp
- Revision:
- 16:cc77770d787f
- Parent:
- 15:e09aaaccf134
diff -r e09aaaccf134 -r cc77770d787f ACS.cpp --- a/ACS.cpp Tue Apr 19 21:27:07 2016 +0000 +++ b/ACS.cpp Fri Jun 03 13:53:55 2016 +0000 @@ -17,6 +17,9 @@ extern uint8_t ACS_MAIN_STATUS; extern uint8_t ACS_STATUS; +extern DigitalOut ATS1_SW_ENABLE; // enable of att sens2 switch +extern DigitalOut ATS2_SW_ENABLE; // enable of att sens switch + extern uint8_t ACS_ATS_ENABLE; extern uint8_t ACS_DATA_ACQ_ENABLE; extern uint8_t ACS_STATE; @@ -60,11 +63,12 @@ void FCTN_ACS_CNTRLALGO(float b[3],float omega[3]) { + float b1[3]; float omega1[3]; b1[0] = b[0]/1000000.0; b1[1] = b[1]/1000000.0; - b1[2] = b[2]/1000000.0; + b1[2] = b[2]/1000000.0; omega1[0] = omega[0]*3.14159/180; omega1[1] = omega[1]*3.14159/180; @@ -314,9 +318,13 @@ I2C i2c (PTC9,PTC8); //PTC9-sda,PTC8-scl for the attitude sensors and battery gauge -void FCTN_ACS_INIT(void); //initialization of registers happens -void FCTN_ATS_DATA_ACQ(); //data is obtained +int FCTN_ACS_INIT(); //initialization of registers happens +int SENSOR_INIT(); +int FCTN_ATS_DATA_ACQ(); //data is obtained +int SENSOR_DATA_ACQ(); void T_OUT(); //timeout function to stop infinite loop + +void CONFIG_UPLOAD(); Timeout to; //Timeout variable to int toFlag; @@ -338,23 +346,58 @@ float senstivity_mag =32.768; //senstivity is obtained from 2^15/1000microtesla float gyro_error[3]= {0,0,0}, mag_error[3]= {0,0,0}; -void FCTN_ACS_INIT() +void CONFIG_UPLOAD() { - ACS_INIT_STATUS = 's'; //set ACS_INIT_STATUS flag - //FLAG(); - pc_acs.printf("Attitude sensor init called \n \r"); - //FLAG(); cmd[0]=RESETREQ; cmd[1]=BIT_RESREQ; i2c.write(SLAVE_ADDR,cmd,2); //When 0x01 is written in reset request register Emulates a hard power down/power up - wait_ms(2000); //waiting for loading configuration file stored in EEPROM + wait_ms(600); + + //Verify magic number + + cmd[0]=HOST_CTRL; //0x02 is written in HOST CONTROL register to enable upload + cmd[1]=BIT_HOST_UPLD_ENB; + i2c.write(SLAVE_ADDR,cmd,2); + wait_ms(100); + + cmd[0]=UPLOAD_ADDR; //0x02 is written in HOST CONTROL register to enable upload + cmd[1]=0x0000; + i2c.write(SLAVE_ADDR,cmd,3); + wait_ms(100); + + + + + cmd[0]=HOST_CTRL; //0x00 is written in HOST CONTROL register to free upload + cmd[1]=0x00; + i2c.write(SLAVE_ADDR,cmd,2); + wait_ms(100); + + + +} + +int SENSOR_INIT() +{ + + pc_acs.printf("Entered sensor init\n \r"); + cmd[0]=RESETREQ; + cmd[1]=BIT_RESREQ; + i2c.write(SLAVE_ADDR,cmd,2); //When 0x01 is written in reset request register Emulates a hard power down/power up + wait_ms(800); //waiting for loading configuration file stored in EEPROM cmd[0]=SENTRALSTATUS; i2c.write(SLAVE_ADDR,cmd,1); i2c.read(SLAVE_ADDR_READ,&store,1); wait_ms(100); + pc_acs.printf("Sentral Status is %x\n \r",(int)store); + //to check whether EEPROM is uploaded switch((int)store) { case(3): { + cmd[0]=RESETREQ; + cmd[1]=BIT_RESREQ; + i2c.write(SLAVE_ADDR,cmd,2); + wait_ms(600); break; } case(11): { @@ -364,50 +407,349 @@ cmd[0]=RESETREQ; cmd[1]=BIT_RESREQ; i2c.write(SLAVE_ADDR,cmd,2); - wait_ms(2000); + wait_ms(600); + } } - pc_acs.printf("Sentral Status is %x\n \r",(int)store); - cmd[0]=HOST_CTRL; //0x01 is written in HOST CONTROL register to enable the sensors - cmd[1]=BIT_RUN_ENB; - i2c.write(SLAVE_ADDR,cmd,2); - wait_ms(100); - cmd[0]=MAGRATE; //Output data rate of 100Hz is used for magnetometer - cmd[1]=BIT_MAGODR; - i2c.write(SLAVE_ADDR,cmd,2); + cmd[0]=SENTRALSTATUS; + i2c.write(SLAVE_ADDR,cmd,1); + i2c.read(SLAVE_ADDR_READ,&store,1); wait_ms(100); - cmd[0]=GYRORATE; //Output data rate of 150Hz is used for gyroscope - cmd[1]=BIT_GYROODR; - i2c.write(SLAVE_ADDR,cmd,2); - wait_ms(100); - cmd[0]=ALGO_CTRL; //When 0x00 is written to ALGO CONTROL register we get scaled sensor values - cmd[1]=0x00; - i2c.write(SLAVE_ADDR,cmd,2); - wait_ms(100); - cmd[0]=ENB_EVT; //enabling the error,gyro values and magnetometer values - cmd[1]=BIT_EVT_ENB; - i2c.write(SLAVE_ADDR,cmd,2); - wait_ms(100); - ACS_INIT_STATUS = 'c'; //set ACS_INIT_STATUS flag + pc_acs.printf("Sentral Status is %x\n \r",(int)store); + + int manual=0; + if((int)store != 11) + { + + cmd[0]=RESETREQ; + cmd[1]=BIT_RESREQ; + i2c.write(SLAVE_ADDR,cmd,2); + wait_ms(600); + + //manually upload + + if(manual == 0) + { + return 0; + } + + } + + cmd[0]=HOST_CTRL; //0x01 is written in HOST CONTROL register to enable the sensors + cmd[1]=BIT_RUN_ENB; + i2c.write(SLAVE_ADDR,cmd,2); + wait_ms(100); + + cmd[0]=MAGRATE; //Output data rate of 100Hz is used for magnetometer + cmd[1]=BIT_MAGODR; + i2c.write(SLAVE_ADDR,cmd,2); + wait_ms(100); + cmd[0]=GYRORATE; //Output data rate of 150Hz is used for gyroscope + cmd[1]=BIT_GYROODR; + i2c.write(SLAVE_ADDR,cmd,2); + wait_ms(100); + cmd[0]=ACCERATE; //Output data rate of 0 Hz is used to disable accelerometer + cmd[1]=0x00; + wait_ms(100); + + i2c.write(SLAVE_ADDR,cmd,2); + wait_ms(100); + cmd[0]=ALGO_CTRL; //When 0x00 is written to ALGO CONTROL register we get scaled sensor values + cmd[1]=0x00; + i2c.write(SLAVE_ADDR,cmd,2); + wait_ms(100); + cmd[0]=ENB_EVT; //enabling the error,gyro values and magnetometer values + cmd[1]=BIT_EVT_ENB; + i2c.write(SLAVE_ADDR,cmd,2); + wait_ms(100); + pc_acs.printf("Exited sensor init successfully\n \r"); + return 1; + + +} +int FCTN_ACS_INIT() +{ + ACS_INIT_STATUS = 1; //set ACS_INIT_STATUS flag + if( (ATS1_SW_ENABLE!= 0 )&&(ATS2_SW_ENABLE!= 0 ) ) + { + ATS2_SW_ENABLE = 1; + ATS1_SW_ENABLE = 0; + wait_ms(5); + ACS_ATS_STATUS = (ACS_ATS_STATUS&0x0F)|0x60; + } + + int working=0; + + pc_acs.printf("Attitude sensor init called \n \r"); + pc_acs.printf("ATS Status is %x\n\n \r",(int)ACS_ATS_STATUS); + pc_acs.printf("ATS Status & 0xC0 is %x\n\n \r",(int)(ACS_ATS_STATUS&0xC0)); + pc_acs.printf("Sensor 1 condition is %d \n\n \r",(int)(( (ACS_ATS_STATUS & 0xC0) != 0xC0)&&( (ACS_ATS_STATUS & 0xC0) != 0x80))); + + + if(( (ACS_ATS_STATUS & 0xC0) != 0xC0)&&( (ACS_ATS_STATUS & 0xC0) != 0x80)) + { + + pc_acs.printf("Sensor 1 marked working \n \r"); + working = SENSOR_INIT(); + if(working ==1) + { + ACS_ATS_STATUS = (ACS_ATS_STATUS&0x0F)|0x60; + pc_acs.printf("ATS Status is %x\n\n \r",(int)ACS_ATS_STATUS); + pc_acs.printf("Attitude sensor init exitting. Init successful. Ideal case.Sensor 1\n \r"); + ACS_INIT_STATUS = 0; + return 1; + } + + + + pc_acs.printf("Sensor 1 not working.Powering off.\n \r"); + ATS1_SW_ENABLE = 1; + ACS_ATS_STATUS = (ACS_ATS_STATUS&0x0F)|0xE0; + + } + + pc_acs.printf("Sensor 1 not working. Trying Sensor 2\n \r"); + + if(( (ACS_ATS_STATUS & 0x0C) != 0x0C)&&( (ACS_ATS_STATUS & 0x0C) != 0x08)) + { + + + ATS2_SW_ENABLE = 0; + wait_ms(5); + working = SENSOR_INIT(); + if(working ==1) + { + pc_acs.printf("ATS Status is %x\n\n \r",(int)ACS_ATS_STATUS); + pc_acs.printf("Attitude sensor init exitting. Init successful. Ideal case.Sensor 2\n \r"); + ACS_ATS_STATUS = (ACS_ATS_STATUS&0xF0)|0x06; + ACS_INIT_STATUS = 0; + return 2; + } + + + } + + pc_acs.printf("ATS Status is %x\n\n \r",(int)ACS_ATS_STATUS); + pc_acs.printf("Sensor 2 also not working.Exit init.\n \r"); + + + + ATS2_SW_ENABLE = 1; + ACS_ATS_STATUS = (ACS_ATS_STATUS&0xF0)|0x0E; + ACS_INIT_STATUS = 0; //set ACS_INIT_STATUS flag + return 0; } -void FCTN_ATS_DATA_ACQ() + +int SENSOR_DATA_ACQ() { - ACS_DATA_ACQ_STATUS = 1; //set ACS_DATA_ACQ_STATUS flag for att sens 2 - if( ACS_ATS_ENABLE == 1) - { - FLAG(); - pc_acs.printf("attitude sensor execution called \n \r"); - toFlag=1; //toFlag is set to 1 so that it enters while loop - to.attach(&T_OUT,2); //after 2 seconds the while loop gets terminated - while(toFlag) { + int mag_only=0; + pc_acs.printf("Entering Sensor data acq.\n \r"); + char reg; + + //int sentral; + int event; + int sensor; + int error; + + int init; cmd[0]=EVT_STATUS; i2c.write(SLAVE_ADDR,cmd,1); i2c.read(SLAVE_ADDR_READ,&status,1); wait_ms(100); pc_acs.printf("Event Status is %x\n \r",(int)status); + event = (int)status; + + cmd[0]=GYRO_XOUT_H; //0x22 gyro LSB of x + i2c.write(SLAVE_ADDR,cmd,1); + i2c.read(SLAVE_ADDR_READ,raw_gyro,6); + cmd[0]=MAG_XOUT_H; //LSB of x + i2c.write(SLAVE_ADDR,cmd,1); + i2c.read(SLAVE_ADDR_READ,raw_mag,6); + // pc_acs.printf("\nGyro Values:\n"); + for(int i=0; i<3; i++) { + //concatenating gyro LSB and MSB to get 16 bit signed data values + bit_data= ((int16_t)raw_gyro[2*i+1]<<8)|(int16_t)raw_gyro[2*i]; + gyro_data[i]=(float)bit_data; + gyro_data[i]=gyro_data[i]/senstivity_gyro; + gyro_data[i]+=gyro_error[i]; + // pc_acs.printf("%f\t",gyro_data[i]); + } + // pc_acs.printf("\nMag Values:\n"); + for(int i=0; i<3; i++) { + //concatenating mag LSB and MSB to get 16 bit signed data values + bit_data= ((int16_t)raw_mag[2*i+1]<<8)|(int16_t)raw_mag[2*i]; + mag_data[i]=(float)bit_data; + mag_data[i]=mag_data[i]/senstivity_mag; + mag_data[i]+=mag_error[i]; + //pc_acs.printf("%f\t",mag_data[i]); + } + for(int i=0; i<3; i++) { + // data[i]=gyro_data[i]; + actual_data.AngularSpeed_actual[i] = gyro_data[i]; + actual_data.Bvalue_actual[i] = mag_data[i]; + //data[i+3]=mag_data[i]; + } + + + + //(event & 40 != 40 ) || (event & 08 != 08 ) || (event & 01 == 01 )|| (event & 02 == 02 ) + + if ( (event & 0x40 != 0x40 ) || (event & 0x08 != 0x08 ) || (event & 0x01 == 0x01 )|| (event & 0x02 == 0x02 )) //check for any error + { + cmd[0]=RESETREQ; + cmd[1]=BIT_RESREQ; + i2c.write(SLAVE_ADDR,cmd,2); + wait_ms(600); + + + + cmd[0]=EVT_STATUS; + i2c.write(SLAVE_ADDR,cmd,1); + i2c.read(SLAVE_ADDR_READ,&status,1); + wait_ms(100); + pc_acs.printf("Event Status after resetting is %x\n \r",(int)status); + + if ( (event & 0x40 != 0x40 ) || (event & 0x08 != 0x08 ) || (event & 0x01 == 0x01 )|| (event & 0x02 == 0x02 )) + { + + + + // cmd[0]=SENTRALSTATUS; + // i2c.write(SLAVE_ADDR,cmd,1); + /// i2c.read(SLAVE_ADDR_READ,®,1); + // wait_ms(100); + // sentral = (int)reg; + + cmd[0]=SENSORSTATUS; + i2c.write(SLAVE_ADDR,cmd,1); + i2c.read(SLAVE_ADDR_READ,®,1); + wait_ms(100); + + sensor = (int)reg; + + cmd[0]=ERROR; + i2c.write(SLAVE_ADDR,cmd,1); + i2c.read(SLAVE_ADDR_READ,®,1); + wait_ms(100); + + error = (int)reg; + + if( error&128 == 128) + { + cmd[0]=MAGRATE; //Output data rate of 100Hz is used for magnetometer + cmd[1]=BIT_MAGODR; + i2c.write(SLAVE_ADDR,cmd,2); + wait_ms(100); + cmd[0]=GYRORATE; //Output data rate of 150Hz is used for gyroscope + cmd[1]=BIT_GYROODR; + i2c.write(SLAVE_ADDR,cmd,2); + wait_ms(100); + cmd[0]=ACCERATE; //Output data rate of 0 Hz is used to disable accelerometer + cmd[1]=0x00; + wait_ms(100); + cmd[0]=ERROR; + i2c.write(SLAVE_ADDR,cmd,1); + i2c.read(SLAVE_ADDR_READ,®,1); + wait_ms(100); + + error = (int)reg; + + if( error&128 == 128) + { + pc_acs.printf("Rate error.Exiting.\n \r"); + return 1; + } + + + } + + + if((error&16 == 16) || (error&32 == 32) || (sensor!=0)) + { + if( (error&1 == 1) || (sensor&1 == 1) || (sensor&16 == 16) ) + { + + if( (error&4 == 4) || (sensor&4 == 4) || (sensor&64 == 64) ) + { + pc_acs.printf("error in both sensors.Exiting.\n \r"); + return 1; + } + pc_acs.printf("error in gyro alone.Exiting.\n \r"); + return 2; + } + pc_acs.printf("error in something else.Exiting.\n \r"); + return 1; + } + + if(((int)status & 1 == 1 )) + { + pc_acs.printf("error in CPU Reset.calling init.\n \r"); + init = SENSOR_INIT(); + if(init == 0) + return 1; + + cmd[0]=EVT_STATUS; + i2c.write(SLAVE_ADDR,cmd,1); + i2c.read(SLAVE_ADDR_READ,&status,1); + wait_ms(100); + if(((int)status & 1 == 1 )) + { + pc_acs.printf("Still error in CPU Reset.Exiting.\n \r"); + return 1; + } + pc_acs.printf("error in CPU Reset cleared.\n \r"); + + } + + if(!(((int)status & 8 == 8 )&&((int)status & 32 == 32 ))) + { + pc_acs.printf("Data not ready waiting...\n \r"); + //POLL + wait_ms(1500); + cmd[0]=EVT_STATUS; + i2c.write(SLAVE_ADDR,cmd,1); + i2c.read(SLAVE_ADDR_READ,&status,1); + wait_ms(100); + if(!(((int)status & 8 == 8 )&&((int)status & 32 == 32 ))) + { + + if((int)status & 32 != 32 ) + { + if((int)status & 8 != 8 ) + { + pc_acs.printf("Both data still not ready.Exiting..\n \r"); + return 1; + } + pc_acs.printf("Mag data only ready.Read..\n \r"); + mag_only = 1; + //return 2; + + } + + + } + + + } + + + } + + + + + + } + + cmd[0]=EVT_STATUS; + i2c.write(SLAVE_ADDR,cmd,1); + i2c.read(SLAVE_ADDR_READ,&status,1); + wait_ms(100); + pc_acs.printf("Event Status is %x\n \r",(int)status); + //if the 6th and 4th bit are 1 then it implies that gyro and magnetometer values are ready to take - if(((int)status&40)==40) { + cmd[0]=GYRO_XOUT_H; //0x22 gyro LSB of x i2c.write(SLAVE_ADDR,cmd,1); i2c.read(SLAVE_ADDR_READ,raw_gyro,6); @@ -438,19 +780,201 @@ actual_data.Bvalue_actual[i] = mag_data[i]; //data[i+3]=mag_data[i]; } - // return(combined_values); //returning poiter combined values - } - //checking for the error - else if (((int)status&2)==2) { - FCTN_ACS_INIT(); //when there is any error then Again inilization is done to remove error + + if(mag_only == 0) + { + + pc_acs.printf("Reading data successful.\n \r"); + return 0; + } + else if(mag_only == 1) + { + pc_acs.printf("Reading data partial success.\n \r"); + return 2; } + + pc_acs.printf("Reading data success.\n \r"); + return 0; + +} + + + +int FCTN_ATS_DATA_ACQ() +{ + + int acq; + + pc_acs.printf("DATA_ACQ called \n \r"); + pc_acs.printf("ATS Status is %x\n\n \r",(int)ACS_ATS_STATUS); + + // 0 success //1 full failure //2 partial failure + + + + if(( (ACS_ATS_STATUS & 0xC0) == 0x40)) + { + + acq = SENSOR_DATA_ACQ(); + if(acq == 0) + { + + ACS_ATS_STATUS = (ACS_ATS_STATUS&0x0F)|0x60; + + ACS_DATA_ACQ_STATUS = 0; //clear ACS_DATA_ACQ_STATUS flag for att sens 2 + pc_acs.printf("ATS Status is %x\n\n \r",(int)ACS_ATS_STATUS); + pc_acs.printf(" Sensor 1 data acq successful.Exit Data ACQ\n \r"); + return 0; + } + else if(acq == 2) + { + ACS_ATS_STATUS = (ACS_ATS_STATUS&0x0F)|0x40; + pc_acs.printf(" Sensor 1 data partial success.Exiting.\n \r"); + return 2; + + /*if((ACS_ATS_STATUS & 0x0F == 0x00)) + { + pc_acs.printf(" Sensor 1 data acq partial success.Trying Sensor 2\n \r"); + ATS1_SW_ENABLE = 1; + ATS2_SW_ENABLE = 0; + wait_ms(5); + ACS_ATS_STATUS = (ACS_ATS_STATUS&0x0F)|0x20; + + int acq; + acq = SENSOR_DATA_ACQ(); + + if(acq == 0) + { + ACS_DATA_ACQ_STATUS = 0; + pc_acs.printf(" Sensor 2 data acq success.Exiting.\n \r"); + return 0; + + } + else if(acq == 2) + { + ACS_DATA_ACQ_STATUS = 2; + pc_acs.printf(" Sensor 2 data acq partial success.Exiting.\n \r"); + return 2; + } + + else if(acq == 1) + { + + int acq; + pc_acs.printf(" Sensor 2 data acq failure.Go to sensor 1 again.\n \r"); + ATS2_SW_ENABLE = 1; + ATS1_SW_ENABLE = 0; + wait_ms(5); + acq = SENSOR_DATA_ACQ(); + if(acq == 0) + { + pc_acs.printf(" Sensor 1 data acq success.Exiting.\n \r"); + ACS_DATA_ACQ_STATUS = 0; + return 0; + } + else if(acq == 2) + { + pc_acs.printf(" Sensor 1 data acq partial success.Exiting.\n \r"); + ACS_DATA_ACQ_STATUS = 2; + return 2; + } + else + { + pc_acs.printf(" Sensor 1 data acq failure.Exiting.\n \r"); + ATS1_SW_ENABLE = 0; + ACS_DATA_ACQ_STATUS = 1; + return 1; + } + + pc_acs.printf(" Sensor 1 data acq failure.Exiting.\n \r"); + ATS1_SW_ENABLE = 0; + ACS_DATA_ACQ_STATUS = 1; + return 1; + + } + + } + + else + { + ACS_ATS_STATUS = (ACS_ATS_STATUS&0x0F)|0x40; + pc_acs.printf(" Sensor 1 data partial success.Sensor 2 marked not working.Exiting.\n \r"); + return 2; + + + }*/ + + } + + else if(acq == 1) + { + pc_acs.printf(" Sensor 1 data acq failure.Try sensor 2.\n \r"); + ATS1_SW_ENABLE = 1; + ACS_ATS_STATUS = (ACS_ATS_STATUS&0x0F)|0xE0; + } + + + } - } - else //ACS_DATA_ACQ_STATUS = ACS_DATA_ACQ_FAILURE + + + + + ACS_ATS_STATUS = (ACS_ATS_STATUS&0x0F)|0xE0; + + + if(( (ACS_ATS_STATUS & 0x0C) == 0x04)) { - ACS_DATA_ACQ_STATUS = 'f'; + ATS2_SW_ENABLE = 0; + wait_ms(5); + + acq = SENSOR_DATA_ACQ(); + if(acq == 0) + { + pc_acs.printf(" Sensor 2 data acq success.Exiting.\n \r"); + ACS_ATS_STATUS = (ACS_ATS_STATUS&0xF0)|0x06; + ACS_DATA_ACQ_STATUS = 0; //clear ACS_DATA_ACQ_STATUS flag for att sens 2 + return 0; + } + else if(acq == 2) + { + + pc_acs.printf(" Sensor 2 data acq partial success.Exiting.\n \r"); + + ACS_ATS_STATUS = (ACS_ATS_STATUS&0xF0)|0x04; + ACS_DATA_ACQ_STATUS = 2; //clear ACS_DATA_ACQ_STATUS flag for att sens 2 + return 2; + + } + + else if(acq == 1) + { + pc_acs.printf(" Sensor 2 data acq failure.Exiting.\n \r"); + ATS2_SW_ENABLE = 1; + ACS_ATS_STATUS = (ACS_ATS_STATUS&0xF0)|0x0E; + //Sensor 2 also not working + } + + + + + } - ACS_DATA_ACQ_STATUS = 0; //clear ACS_DATA_ACQ_STATUS flag for att sens 2 + + pc_acs.printf(" Reading value from sensor 1 before exiting\n \r"); + ATS1_SW_ENABLE = 0; + wait_ms(5); + SENSOR_DATA_ACQ(); + ATS1_SW_ENABLE = 1; + wait_ms(5); + + ACS_ATS_STATUS = (ACS_ATS_STATUS&0xF0)|0x0E; + + pc_acs.printf("ATS Status is %x\n\n \r",(int)ACS_ATS_STATUS); + pc_acs.printf(" Both sensors data acq failure.Exiting.\n \r"); + + ACS_DATA_ACQ_STATUS = 1; //set ACS_DATA_ACQ_STATUS flag for att sens 2 + return 1; } void FCTN_ACS_GENPWM_MAIN(float Moment[3])