Team Fox
FINAL ACS TO BE USED FOR TESTING. COMMISSIONING, ACS MAIN, DATA ACQ ALL DONE.
Dependencies: FreescaleIAP mbed-rtos mbed
Fork of
ACS_FULL_Flowchart_BAE
by 
Team Fox
ACS.cpp
- Committer:
- Bragadeesh153
- Date:
- 2016-06-13
- Revision:
- 18:21740620c65e
- Parent:
- 17:1e1955f3db75
- Child:
- 19:403cb36e22ed
File content as of revision 18:21740620c65e:
/*------------------------------------------------------------------------------------------------------------------------------------------------------
-------------------------------------------CONTROL ALGORITHM------------------------------------------------------------------------------------------*/
#include <mbed.h>
#include <math.h>
#include "pni.h" //pni header file
#include "pin_config.h"
#include "ACS.h"
#include "EPS.h"
//********************************flags******************************************//
extern uint32_t BAE_STATUS;
extern uint32_t BAE_ENABLE;
extern uint8_t ACS_INIT_STATUS;
extern uint8_t ACS_DATA_ACQ_STATUS;
extern uint8_t ACS_ATS_STATUS;
extern uint8_t ACS_MAIN_STATUS;
extern uint8_t ACS_STATUS;
extern uint8_t ACS_DETUMBLING_ALGO_TYPE;
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;
DigitalOut phase_TR_x(PIN27); // PHASE pin for x-torquerod
DigitalOut phase_TR_y(PIN28); // PHASE pin for y-torquerod
DigitalOut phase_TR_z(PIN86); // PHASE pin for z-torquerod
extern PwmOut PWM1; //x //Functions used to generate PWM signal
extern PwmOut PWM2; //y
extern PwmOut PWM3; //z //PWM output comes from pins p6
int g_err_flag_TR_x=0; // setting x-flag to zero
int g_err_flag_TR_y=0; // setting y-flag to zero
int g_err_flag_TR_z=0; // setting z-flag to zero
extern float data[6];
extern BAE_HK_actual actual_data;
Serial pc_acs(USBTX,USBRX); //for usb communication
//CONTROL_ALGO
float moment[3]; // Unit: Ampere*Meter^2
float b_old[3]={1.15e-5,-0.245e-5,1.98e-5}; // Unit: Tesla
float db[3];
uint8_t flag_firsttime=1, alarmmode=0;
void controlmodes(float b[3], float db[3], float omega[3], uint8_t controlmode1);
float max_array(float arr[3]);
void inverse(float mat[3][3],float inv[3][3]);
//CONTROLALGO PARAMETERS
void FCTN_ACS_CNTRLALGO ( float b[3] , float omega[3],int nominal)
{
float normalising_fact;
float b_copy[3], omega_copy[3], db_copy[3];
int i;
if(flag_firsttime==1)
{
for(i=0;i<3;i++)
{
db[i]=0; // Unit: Tesla/Second
}
flag_firsttime=0;
}
else
{
for(i=0;i<3;i++)
{
db[i]= (b[i]-b_old[i])/sampling_time; // Unit: Tesla/Second
}
}
if(nominal == 0)
{
if(max_array(omega)<(0.8*OmegaMax) && alarmmode==1)
{
alarmmode=0;
}
else if(max_array(omega)>OmegaMax&& alarmmode==0)
{
alarmmode=1;
}
}
for (i=0;i<3;i++)
{
b_copy[i]=b[i];
db_copy[i]=db[i];
omega_copy[i]=omega[i];
}
if((alarmmode==0)|| (nominal == 1))
{
controlmodes(b,db,omega,0);
for (i=0;i<3;i++)
{
b[i]=b_copy[i];
db[i]=db_copy[i];
omega[i]=omega_copy[i];
}
if(max_array(moment)>MmntMax)
{
controlmodes(b,db,omega,1);
for (i=0;i<3;i++)
{
b[i]=b_copy[i];
db[i]=db_copy[i];
omega[i]=omega_copy[i];
}
if(max_array(moment)>MmntMax)
{
normalising_fact=max_array(moment)/MmntMax;
for(i=0;i<3;i++)
{
moment[i]/=normalising_fact; // Unit: Ampere*Meter^2
}
}
}
ACS_STATUS = 5;
}
else
{
controlmodes(b,db,omega,1);
for (i=0;i<3;i++)
{
b[i]=b_copy[i];
db[i]=db_copy[i];
omega[i]=omega_copy[i];
}
if(max_array(moment)>MmntMax)
{
normalising_fact=max_array(moment)/MmntMax;
for(i=0;i<3;i++)
{
moment[i]/=normalising_fact; // Unit: Ampere*Meter^2
}
}
}
for (i=0;i<3;i++)
{
b_old[i]=b[i];
}
}
void inverse(float mat[3][3],float inv[3][3],int &singularity_flag)
{
int i,j;
float det=0;
for(i=0;i<3;i++)
{
for(j=0;j<3;j++)
{
inv[j][i]=(mat[(i+1)%3][(j+1)%3]*mat[(i+2)%3][(j+2)%3])-(mat[(i+2)%3][(j+1)%3]*mat[(i+1)%3][(j+2)%3]);
}
}
det+=(mat[0][0]*inv[0][0])+(mat[0][1]*inv[1][0])+(mat[0][2]*inv[2][0]);
if (det==0)
{
singularity_flag=1;
}
else
{
singularity_flag=0;
for(i=0;i<3;i++)
{
for(j=0;j<3;j++)
{
inv[i][j]/=det;
}
}
}
}
float max_array(float arr[3])
{
int i;
float temp_max=fabs(arr[0]);
for(i=1;i<3;i++)
{
if(fabs(arr[i])>temp_max)
{
temp_max=fabs(arr[i]);
}
}
return temp_max;
}
void controlmodes(float b[3], float db[3], float omega[3], uint8_t controlmode1)
{
float bb[3]={0,0,0};
float d[3]={0,0,0};
float Jm[3][3]={{0.2271,0.0014,-0.0026},{0.0014,0.2167,-0.004},{-0.0026,-0.004,0.2406}}; // Unit: Kilogram*Meter^2. Jm may change depending on the final satellite structure
float den=0,den2;
float bcopy[3];
int i, j;//temporary variables
float Mu[2],z[2],dv[2],v[2],u[2],tauc[3]={0,0,0},Mmnt[3];//outputs
float invJm[3][3];
float kmu2=0.07,gamma2=1.9e4,kz2=0.4e-2,kmu=0.003,gamma=5.6e4,kz=0.1e-4;
int singularity_flag=0;
if(controlmode1==0)
{
den=sqrt((b[0]*b[0])+(b[1]*b[1])+(b[2]*b[2]));
den2=(b[0]*db[0])+(b[1]*db[1])+(b[2]*db[2]);
if (den==0)
{
singularity_flag=1;
}
if (singularity_flag==0)
{
for(i=0;i<3;i++)
{
db[i]=((db[i]*den*den)-(b[i]*(den2)))/(pow(den,3)); // Normalized db. Hence the unit is Second^(-1)
}
for(i=0;i<3;i++)
{
b[i]/=den; // Mormalized b. Hence no unit.
}
if(b[2]>0.9 || b[2]<-0.9)
{
kz=kz2;
kmu=kmu2;
gamma=gamma2;
}
for(i=0;i<2;i++)
{
Mu[i]=b[i];
v[i]=-kmu*Mu[i];
dv[i]=-kmu*db[i];
z[i]=db[i]-v[i];
u[i]=-kz*z[i]+dv[i]-(Mu[i]/gamma);
}
inverse(Jm,invJm,singularity_flag);
for(i=0;i<3;i++)
{
for(j=0;j<3;j++)
{
bb[i]+=omega[j]*(omega[(i+1)%3]*Jm[(i+2)%3][j]-omega[(i+2)%3]*Jm[(i+1)%3][j]);
}
}
for(i=0;i<3;i++)
{
for(j=0;j<3;j++)
{
d[i]+=bb[j]*invJm[i][j];
}
}
bb[1]=u[0]-(d[1]*b[2])+(d[2]*b[1])-(omega[1]*db[2])+(omega[2]*db[1]);
bb[2]=u[1]-(d[2]*b[0])+(d[0]*b[2])-(omega[2]*db[0])+(omega[0]*db[2]);
bb[0]=0;
for(i=0;i<3;i++)
{
d[i]=invJm[2][i];
invJm[1][i]=-b[2]*invJm[1][i]+b[1]*d[i];
invJm[2][i]=b[2]*invJm[0][i]-b[0]*d[i];
invJm[0][i]=b[i];
}
inverse(invJm,Jm,singularity_flag);
if (singularity_flag==0)
{
for(i=0;i<3;i++)
{
for(j=0;j<3;j++)
{
tauc[i]+=Jm[i][j]*bb[j]; // Unit: Newton*Meter^2
}
}
for(i=0;i<3;i++)
{
bcopy[i]=b[i]*den;
}
for(i=0;i<3;i++)
{
Mmnt[i]=bcopy[(i+1)%3]*tauc[(i+2)%3]-bcopy[(i+2)%3]*tauc[(i+1)%3];
Mmnt[i]/=(den*den); // Unit: Ampere*Meter^2
}
}
}
if (singularity_flag==1)
{
for (i=0;i<3;i++)
{
Mmnt[i]=2*MmntMax;
}
}
}
else if(controlmode1==1)
{
if (ACS_DETUMBLING_ALGO_TYPE==0) // BOmega Algo
{
for(i=0;i<3;i++)
{
Mmnt[i]=-kdetumble*(b[(i+1)%3]*omega[(i+2)%3]-b[(i+2)%3]*omega[(i+1)%3]); // Unit: Ampere*Meter^2
}
ACS_STATUS = 6;
}
else if(ACS_DETUMBLING_ALGO_TYPE==1) // BDot Algo
{
for(i=0;i<3;i++)
{
Mmnt[i]=-kdetumble*db[i];
}
ACS_STATUS = 4;
}
}
for(i=0;i<3;i++)
{
moment[i]=Mmnt[i]; // Unit: Ampere*Meter^2
}
}
I2C i2c (PTC9,PTC8); //PTC9-sda,PTC8-scl for the attitude sensors and battery gauge
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
int CONFIG_UPLOAD();
Timeout to; //Timeout variable to
int toFlag;
int count =0; // Time for which the BAE uC is running (in seconds)
void T_OUT()
{
toFlag=0; //as T_OUT function gets called the while loop gets terminated
}
//DEFINING VARIABLES
char cmd[2];
char raw_gyro[6];
char raw_mag[6];
char reg_data[24];
char store,status;
int16_t bit_data;
uint16_t time_data;
float gyro_data[3], mag_data[3];
float gyro_error[3]= {0,0,0}, mag_error[3]= {0,0,0};
int CONFIG_UPLOAD()
{
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(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);
return 0;
}
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(600); //waiting for loading configuration file stored in EEPROM
cmd[0]=SENTRALSTATUS;
i2c.write(SLAVE_ADDR,cmd,1);
i2c.read(SLAVE_ADDR_READ,&store,1);
pc_acs.printf("Sentral Status is %x\n \r",(int)store);
//to check whether EEPROM is uploaded properly
switch((int)store) {
case(3): {
break;
}
case(11): {
break;
}
default: {
cmd[0]=RESETREQ;
cmd[1]=BIT_RESREQ;
i2c.write(SLAVE_ADDR,cmd,2);
wait_ms(600);
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);
}
}
int manual=0;
if( ((int)store != 11 )&&((int)store != 11))
{
cmd[0]=RESETREQ;
cmd[1]=BIT_RESREQ;
i2c.write(SLAVE_ADDR,cmd,2);
wait_ms(600);
manual = CONFIG_UPLOAD();
if(manual == 0)
{
//MANUAL CONFIGURATION FAILED
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);
cmd[0]=MAGRATE; //Output data rate of 100Hz is used for magnetometer
cmd[1]=BIT_MAGODR;
i2c.write(SLAVE_ADDR,cmd,2);
cmd[0]=GYRORATE; //Output data rate of 150Hz is used for gyroscope
cmd[1]=BIT_GYROODR;
i2c.write(SLAVE_ADDR,cmd,2);
cmd[0]=ACCERATE; //Output data rate of 0 Hz is used to disable accelerometer
cmd[1]=0x00;
i2c.write(SLAVE_ADDR,cmd,2);
wait_ms(100);
cmd[0]=ALGO_CTRL; //When 0x00 is written to ALGO CONTROL register , to scaled sensor values
cmd[1]=0x00;
i2c.write(SLAVE_ADDR,cmd,2);
cmd[0]=ENB_EVT; //Enabling the CPU reset , error,gyro values and magnetometer values
cmd[1]=BIT_EVT_ENB;
i2c.write(SLAVE_ADDR,cmd,2);
cmd[0]=SENTRALSTATUS;
i2c.write(SLAVE_ADDR,cmd,1);
i2c.read(SLAVE_ADDR_READ,&store,1);
pc_acs.printf("Sentral Status after initialising is %x\n \r",(int)store);
if( (int)store == 3) //Check if initialised properly and not in idle state
{
pc_acs.printf("Exited sensor init successfully\n \r");
return 1;
}
else if((int)store == 11)
{
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);
cmd[0]=SENTRALSTATUS;
i2c.write(SLAVE_ADDR,cmd,1);
i2c.read(SLAVE_ADDR_READ,&store,1);
wait_ms(100);
pc_acs.printf("Sentral Status after trying again is %x\n \r",(int)store);
if( (int)store != 3)
{
pc_acs.printf("Problem with initialising\n \r");
return 0;
}
}
pc_acs.printf("Sensor init failed \n \r") ;
return 0;
}
int FCTN_ACS_INIT()
{
ACS_INIT_STATUS = 1; //set ACS_INIT_STATUS flag
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);
if(( (ACS_ATS_STATUS & 0xC0) != 0xC0)&&( (ACS_ATS_STATUS & 0xC0) != 0x80)) //Sensor1 status is not 10 or 11
{
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); //Sensor 1 INIT successful
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"); //Sensor 1 INIT failure and power off
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)) //Sensor1 status is not 10 or 11
{
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"); //Sensor2 INIT successful
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 //Sensor 2 also not working
return 0;
}
int SENSOR_DATA_ACQ()
{
int mag_only=0;
pc_acs.printf("Entering Sensor data acq.\n \r");
char status;
int sentral;
int event;
int sensor;
int error;
int init;
int ack1;
int ack2;
cmd[0]=EVT_STATUS;
i2c.write(SLAVE_ADDR,cmd,1);
ack1 = i2c.read(SLAVE_ADDR_READ,&status,1);
//wait_ms(100);
event = (int)status;
cmd[0]=SENTRALSTATUS;
i2c.write(SLAVE_ADDR,cmd,1);
ack2 = i2c.read(SLAVE_ADDR_READ,&status,1);
printf("Ack1: %d Ack2 : %d\n",ack1,ack2);
if((ack1!=0)||(ack2!=0))
{
cmd[0]=EVT_STATUS;
i2c.write(SLAVE_ADDR,cmd,1);
ack1 = i2c.read(SLAVE_ADDR_READ,&status,1);
//wait_ms(100);
cmd[0]=SENTRALSTATUS;
i2c.write(SLAVE_ADDR,cmd,1);
ack2 = i2c.read(SLAVE_ADDR_READ,&status,1);
if((ack1!=0)||(ack2!=0))
{
for(int i=0; i<3; i++) {
actual_data.AngularSpeed_actual[i] = 0; //acknowledgement failed
actual_data.Bvalue_actual[i] = 0;
}
return 1;
}
}
sentral = (int) status;
pc_acs.printf("Event Status is %x\n \r",event);
pc_acs.printf("Sentral Status is %x\n \r",sentral);
if ( (event & 0x40 != 0x40 ) || (event & 0x08 != 0x08 ) || (event & 0x01 == 0x01 )|| (event & 0x02 == 0x02 )|| (sentral!= 3)) //check for any error in event status register
{
init = SENSOR_INIT();
int ack1,ack2;
cmd[0]=EVT_STATUS;
i2c.write(SLAVE_ADDR,cmd,1);
ack1 = i2c.read(SLAVE_ADDR_READ,&status,1);
//wait_ms(100);
event = (int)status;
cmd[0]=SENTRALSTATUS;
i2c.write(SLAVE_ADDR,cmd,1);
ack2 = i2c.read(SLAVE_ADDR_READ,&status,1);
sentral = (int)status;
if((ack1!=0)||(ack2!=0))
{
cmd[0]=EVT_STATUS;
i2c.write(SLAVE_ADDR,cmd,1);
ack1 = i2c.read(SLAVE_ADDR_READ,&status,1);
event = (int)status;
wait_ms(100);
cmd[0]=SENTRALSTATUS;
i2c.write(SLAVE_ADDR,cmd,1);
ack2 = i2c.read(SLAVE_ADDR_READ,&status,1);
sentral = (int)status;
wait_ms(100);
if((ack1!=0)||(ack2!=0))
{
for(int i=0; i<3; i++) {
actual_data.AngularSpeed_actual[i] = 0; //acknowledgement failed
actual_data.Bvalue_actual[i] = 0;
}
return 1;
}
}
pc_acs.printf("Event Status after resetting and init is %x\n \r",event);
if ( (event & 0x40 != 0x40 ) || (event & 0x08 != 0x08) || (event & 0x01 == 0x01 )|| (event & 0x02 == 0x02 ) || (init == 0)||(sentral != 3)) //check for any error in event status
{
int ack1,ack2;
char status;
cmd[0]=ERROR;
i2c.write(SLAVE_ADDR,cmd,1);
ack1 = i2c.read(SLAVE_ADDR_READ,&status,1);
error = (int)status;
cmd[0]=SENSORSTATUS;
i2c.write(SLAVE_ADDR,cmd,1);
ack2 = i2c.read(SLAVE_ADDR_READ,&status,1);
sensor = (int)status;
if((ack1!=0)||(ack2!=0))
{
cmd[0]=ERROR;
i2c.write(SLAVE_ADDR,cmd,1);
ack1 = i2c.read(SLAVE_ADDR_READ,&status,1);
error = (int)status;
wait_ms(100);
cmd[0]=SENSORSTATUS;
i2c.write(SLAVE_ADDR,cmd,1);
ack2 = i2c.read(SLAVE_ADDR_READ,&status,1);
sensor = (int)status;
wait_ms(100);
if((ack1!=0)||(ack2!=0))
{
for(int i=0; i<3; i++) {
actual_data.AngularSpeed_actual[i] = 0; //acknowledgement failed
actual_data.Bvalue_actual[i] = 0;
}
return 1;
}
}
if((error!=0) || (sensor!=0))
{
if( (error&1 == 1) || (sensor&1 == 1) || (sensor&16 == 16) )
{
if( (error&4 == 4) || (sensor&4 == 4) || (sensor&64 == 64) )
{
for(int i=0; i<3; i++) {
actual_data.AngularSpeed_actual[i] = 0; //Set values to 0
actual_data.Bvalue_actual[i] = 0;
}
pc_acs.printf("error in both sensors.Exiting.\n \r");
return 1;
}
pc_acs.printf("error in gyro alone.Exiting.\n \r");
for(int i=0; i<3; i++) {
actual_data.AngularSpeed_actual[i] = 0; //Set values to 0
}
mag_only = 1;
//return 2;
}
if(mag_only!= 1){
pc_acs.printf("error in something else.Exiting.\n \r");
for(int i=0; i<3; i++) {
actual_data.AngularSpeed_actual[i] = 0; //Set values to 0
actual_data.Bvalue_actual[i] = 0;
}
return 1;
}
}
if((event & 1 == 1 ))
{
pc_acs.printf("error in CPU Reset.\n \r");
for(int i=0; i<3; i++) {
actual_data.AngularSpeed_actual[i] = 0; //Set values to 0
actual_data.Bvalue_actual[i] = 0;
}
return 1;
}
if((event & 8 != 8 )||(event & 32 != 32 ))
{
pc_acs.printf("Data not ready waiting...\n \r");
//POLL
wait_ms(1000);
cmd[0]=EVT_STATUS;
i2c.write(SLAVE_ADDR,cmd,1);
i2c.read(SLAVE_ADDR_READ,&status,1);
wait_ms(100);
if((event & 8 != 8 )||(event & 32 != 32 ))
{
if(event & 32 != 32 )
{
if(event & 8 != 8 )
{
pc_acs.printf("Both data still not ready.Exiting..\n \r");
for(int i=0; i<3; i++) {
actual_data.AngularSpeed_actual[i] = 0; //Set values to 0
actual_data.Bvalue_actual[i] = 0;
}
return 1;
}
pc_acs.printf("Mag data only ready.Read..\n \r");
mag_only = 1;
//return 2;
}
}
}
}
if(mag_only !=1)
{
if(mag_only!= 1){
pc_acs.printf("Error in something else.Exiting.\n \r");
for(int i=0; i<3; i++) {
actual_data.AngularSpeed_actual[i] = 0; //Set values to 0
actual_data.Bvalue_actual[i] = 0;
}
return 1;
}
}
}
cmd[0]=MAG_XOUT_H; //LSB of x
i2c.write(SLAVE_ADDR,cmd,1); //Read gryo and mag registers together
ack1 = i2c.read(SLAVE_ADDR_READ,reg_data,24);
if(ack1 != 0)
{
wait_ms(100);
cmd[0]=MAG_XOUT_H; //LSB of x
i2c.write(SLAVE_ADDR,cmd,1); //Read gryo and mag registers together
ack1 = i2c.read(SLAVE_ADDR_READ,reg_data,24);
wait_ms(100);
if(ack1 !=1)
{
for(int i=0;i<3;i++)
{
actual_data.Bvalue_actual[i] = 0;
actual_data.AngularSpeed_actual[i] = 0;
}
return 1;
}
}
// 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)reg_data[16+2*i+1]<<8)|(int16_t)reg_data[16+2*i];
gyro_data[i]=(float)bit_data;
gyro_data[i]=gyro_data[i]/senstivity_gyro;
gyro_data[i]+=gyro_error[i];
}
for(int i=0; i<3; i++) {
//concatenating mag LSB and MSB to get 16 bit signed data values Extract data
bit_data= ((int16_t)reg_data[2*i+1]<<8)|(int16_t)reg_data[2*i];
mag_data[i]=(float)bit_data;
mag_data[i]=mag_data[i]/senstivity_mag;
mag_data[i]+=mag_error[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];
}
if(mag_only == 0)
{
pc_acs.printf("Reading data successful.\n \r");
return 0;
}
else if(mag_only == 1)
{
for(int i=0;i<3;i++)
{
actual_data.AngularSpeed_actual[i] = 0;
}
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;
}
}
ACS_ATS_STATUS = (ACS_ATS_STATUS&0x0F)|0xE0;
if(( (ACS_ATS_STATUS & 0x0C) == 0x04))
{
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_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])
{
printf("\n\rEntered executable PWMGEN function\n"); // entering the PWMGEN executable function
float l_duty_cycle_x=0; //Duty cycle of Moment in x direction
float l_current_x=0; //Current sent in x TR's
float l_duty_cycle_y=0; //Duty cycle of Moment in y direction
float l_current_y=0; //Current sent in y TR's
float l_duty_cycle_z=0; //Duty cycle of Moment in z direction
float l_current_z=0; //Current sent in z TR's
printf("\r\r");
//----------------------------- x-direction TR --------------------------------------------//
float l_moment_x = Moment[0]; //Moment in x direction
phase_TR_x = 1; // setting the default current direction
if (l_moment_x <0)
{
phase_TR_x = 0; // if the moment value is negative, we send the abs value of corresponding current in opposite direction by setting the phase pin high
l_moment_x = abs(l_moment_x);
}
l_current_x = l_moment_x * TR_CONSTANT ; //Moment and Current always have the linear relationship
printf("current in trx is %f \r \n",l_current_x);
if( l_current_x>0 && l_current_x < 0.0016 ) //Current and Duty cycle have the linear relationship between 1% and 100%
{
l_duty_cycle_x = 3*10000000*pow(l_current_x,3)- 90216*pow(l_current_x,2) + 697.78*l_current_x - 0.0048; // calculating upto 0.1% dutycycle by polynomial interpolation
printf("DC for trx is %f \r \n",l_duty_cycle_x);
PWM1.period(TIME_PERIOD);
PWM1 = l_duty_cycle_x/100 ;
}
else if (l_current_x >= 0.0016 && l_current_x < 0.0171)
{
l_duty_cycle_x = - 76880*pow(l_current_x,3) + 1280.8*pow(l_current_x,2) + 583.78*l_current_x + 0.0281; // calculating upto 10% dutycycle by polynomial interpolation
printf("DC for trx is %f \r \n",l_duty_cycle_x);
PWM1.period(TIME_PERIOD);
PWM1 = l_duty_cycle_x/100 ;
}
else if(l_current_x >= 0.0171 && l_current_x < 0.1678)
{
l_duty_cycle_x = 275.92*pow(l_current_x,2) + 546.13*l_current_x + 0.5316; // calculating upto 100% dutycycle by polynomial interpolation
printf("DC for trx is %f \r \n",l_duty_cycle_x);
PWM1.period(TIME_PERIOD);
PWM1 = l_duty_cycle_x/100 ;
}
else if(l_current_x==0)
{
printf("\n \r l_current_x====0");
l_duty_cycle_x = 0; // default value of duty cycle
printf("DC for trx is %f \r \n",l_duty_cycle_x);
PWM1.period(TIME_PERIOD);
PWM1 = l_duty_cycle_x/100 ;
}
else //not necessary
{
g_err_flag_TR_x = 1;
}
//------------------------------------- y-direction TR--------------------------------------//
float l_moment_y = Moment[1]; //Moment in y direction
phase_TR_y = 1; // setting the default current direction
if (l_moment_y <0)
{
phase_TR_y = 0; //if the moment value is negative, we send the abs value of corresponding current in opposite direction by setting the phase pin high
l_moment_y = abs(l_moment_y);
}
l_current_y = l_moment_y * TR_CONSTANT ; //Moment and Current always have the linear relationship
printf("current in try is %f \r \n",l_current_y);
if( l_current_y>0 && l_current_y < 0.0016 ) //Current and Duty cycle have the linear relationship between 1% and 100%
{
l_duty_cycle_y = 3*10000000*pow(l_current_y,3)- 90216*pow(l_current_y,2) + 697.78*l_current_y - 0.0048; // calculating upto 0.1% dutycycle by polynomial interpolation
printf("DC for try is %f \r \n",l_duty_cycle_y);
PWM2.period(TIME_PERIOD);
PWM2 = l_duty_cycle_y/100 ;
}
else if (l_current_y >= 0.0016 && l_current_y < 0.0171)
{
l_duty_cycle_y = - 76880*pow(l_current_y,3) + 1280.8*pow(l_current_y,2) + 583.78*l_current_y + 0.0281; // calculating upto 10% dutycycle by polynomial interpolation
printf("DC for try is %f \r \n",l_duty_cycle_y);
PWM2.period(TIME_PERIOD);
PWM2 = l_duty_cycle_y/100 ;
}
else if(l_current_y >= 0.0171 && l_current_y < 0.1678)
{
l_duty_cycle_y = 275.92*pow(l_current_y,2) + 546.13*l_current_y + 0.5316; // calculating upto 100% dutycycle by polynomial interpolation
printf("DC for try is %f \r \n",l_duty_cycle_y);
PWM2.period(TIME_PERIOD);
PWM2 = l_duty_cycle_y/100 ;
}
else if(l_current_y==0)
{
printf("\n \r l_current_y====0");
l_duty_cycle_y = 0; // default value of duty cycle
printf("DC for try is %f \r \n",l_duty_cycle_y);
PWM2.period(TIME_PERIOD);
PWM2 = l_duty_cycle_y/100 ;
}
else // not necessary
{
g_err_flag_TR_y = 1;
}
//----------------------------------------------- z-direction TR -------------------------//
float l_moment_z = Moment[2]; //Moment in z direction
phase_TR_z = 1; // setting the default current direction
if (l_moment_z <0)
{
phase_TR_z = 0; //if the moment value is negative, we send the abs value of corresponding current in opposite direction by setting the phase pin high
l_moment_z = abs(l_moment_z);
}
l_current_z = l_moment_z * TR_CONSTANT ; //Moment and Current always have the linear relationship
printf("current in trz is %f \r \n",l_current_z);
if( l_current_z>0 && l_current_z < 0.0016 ) //Current and Duty cycle have the linear relationship between 1% and 100%
{
l_duty_cycle_z = 3*10000000*pow(l_current_z,3)- 90216*pow(l_current_z,2) + 697.78*l_current_z - 0.0048; // calculating upto 0.1% dutycycle by polynomial interpolation
printf("DC for trz is %f \r \n",l_duty_cycle_z);
PWM3.period(TIME_PERIOD);
PWM3 = l_duty_cycle_z/100 ;
}
else if (l_current_z >= 0.0016 && l_current_z < 0.0171)
{
l_duty_cycle_z = - 76880*pow(l_current_z,3) + 1280.8*pow(l_current_z,2) + 583.78*l_current_z + 0.0281; // calculating upto 10% dutycycle by polynomial interpolation
printf("DC for trz is %f \r \n",l_duty_cycle_z);
PWM3.period(TIME_PERIOD);
PWM3 = l_duty_cycle_z/100 ;
}
else if(l_current_z >= 0.0171 && l_current_z < 0.1678)
{
l_duty_cycle_z = 275.92*pow(l_current_z,2) + 546.13*l_current_z + 0.5316; // calculating upto 100% dutycycle by polynomial interpolation
printf("DC for trz is %f \r \n",l_duty_cycle_z);
PWM3.period(TIME_PERIOD);
PWM3 = l_duty_cycle_z/100 ;
}
else if(l_current_z==0)
{
printf("\n \r l_current_z====0");
l_duty_cycle_z = 0; // default value of duty cycle
printf("DC for trz is %f \r \n",l_duty_cycle_z);
PWM3.period(TIME_PERIOD);
PWM3 = l_duty_cycle_z/100 ;
}
else // not necessary
{
g_err_flag_TR_z = 1;
}
//-----------------------------------------exiting the function-----------------------------------//
printf("\n\rExited executable PWMGEN function\n\r"); // stating the successful exit of TR function
}