#include "C:\Users\Honza\Documents\pic\azimut\main.h"
#define PIN_SDA PIN_C4
#define PIN_SCL PIN_C3
#use i2c(master, sda=PIN_SDA, scl=PIN_SCL)
#use rs232(baud=9600,parity=N,xmit=PIN_C7,rcv=PIN_C6,bits=8) //rcv TXD xmit RXD
#include <math.h>
#include <stdio.h>
//#include "sscanf.c"
#include <stdlib.h>
#include <input.c>
#include <string.h>
//Akcelerometr
#define AK_W 0x38 //adresa akcelerometru zápis
#define AK_R 0x39 //adresa akcelerometru ètení
#define AK_XH 0x01 //osa X LSB
#define AK_XL 0x02 //osa X MSB
#define AK_YH 0x03 //osa Y LSB
#define AK_YL 0x04 //osa Y MSB
#define AK_ZH 0x05 //osa Z LSB
#define AK_ZL 0x06 //osa Z MSB
//Magnetometr
#define MAG_W 0x3C //adresa akcelerometru zápis
#define MAG_R 0x3D //adresa akcelerometru ètení
#define MAG_XH 0x03 //osa X LSB
#define MAG_XL 0x04 //osa X MSB
#define MAG_ZH 0x05 //osa Y LSB
#define MAG_ZL 0x06 //osa Y MSB
#define MAG_YH 0x07 //osa Z LSB
#define MAG_YL 0x08 //osa Z MSB
//pøipojení motorù
//AIN1 - pro vysku slunce
#define AIN1 PIN_D0
#define AIN2 PIN_D1
//motor A -cerveny vodic na AOUT1
//motor A -modry vodic na Aout2
//AIN2 - pro azimut
#define BIN1 PIN_D2
#define BIN2 PIN_D3
//motor B - èerveny vodic na BOUT2
//motor B - modrý vodic na BOUT1
signed int16 X, Y, Z,AX, AY, AZ; //promenne pro magnetometr a akcelerometr
unsigned int16 azimutZAD, elevaceZAD;
void setAK (void) //nastaveni akcelerometru
{
i2c_start();
I2C_Write(AK_W);
I2C_write(0x2A);
I2C_write(0x01); //nastaví aktivní stav
i2c_stop();
}
void setmag (void)
{
i2c_start();
I2C_Write(MAG_W); // W
I2C_Write(0x00);
I2C_Write(0x78);
i2c_stop();
Delay_ms(6);
i2c_start();
I2C_Write(MAG_W); // W
I2C_Write(0x01);
I2C_Write(0x00);
i2c_stop();
Delay_ms(6);
i2c_start();
I2C_Write(MAG_W); // W
I2C_Write(0x02);
I2C_Write(0x00);
i2c_stop();
Delay_ms(6);
}
int16 akR (int8 H, int8 L) //vycitani hodnot z akcelerometru
{
unsigned int8 XL=0,XH=0;
signed int16 x;
i2c_start();
I2C_Write(AK_W);
I2C_write(H);
i2c_start();
I2C_Write(AK_R);
XH=i2c_read(0);
i2c_stop();
i2c_start();
I2C_Write(AK_W);
I2C_write(L);
i2c_start();
I2C_Write(AK_R);
XL=i2c_read(0);
i2c_stop();
x = (((unsigned int16) XH << 8) + XL ); //prevod na 16bit hodnotu
x=x/4;
return x;
}
int16 magR (int8 H, int8 L) //vycitani hodnot z magnetometru
{
unsigned int8 XL=0,XH=0;
signed int16 x;
i2c_start();
I2C_Write(MAG_W);
I2C_write(H);
i2c_start();
I2C_Write(MAG_R);
XH=i2c_read(0);
i2c_stop();
i2c_start();
I2C_Write(MAG_W);
I2C_write(L);
i2c_start();
I2C_Write(MAG_R);
XL=i2c_read(0);
i2c_stop();
x = (((unsigned int16) XH << 8) + XL );
return x;
}
float elevace (void) //vypocet aktualni elevace panelu
{
//printf("Akcelerometr5: \r\n",);
X= akR (AK_XH, AK_XL);
Y= akR (AK_YH, AK_YL);
Z= akR (AK_ZH, AK_ZL);
AX=abs(X);
AY=abs(Y)+250;
AZ=abs(Z)+250;
float a, b;
a=(float)Y/Z;
b=atan(a);
b = (b/3.14)*180;
b=abs(b);
if(((AX>AY) || (AX>AZ))) //indikace prevraceni panelu
{
printf("Prevracený panel)\r\n", );
}
else
{
if(Z==0) //osetreni proti deleni 0
{
if(Y>0)
{
b=180;
}
else
{
b=0;
}
}
else
{
if(Z>0)
{
if(Y>=0)
{
b=90+b;
}
else
{
b=90-b;
}
}
else
{
if(Y>=0)
{
b=180-b;
}
else
{
b=270+b;
}
}
}
}
// printf("uhel namìreny %10.2f \r\n", b);
if(b>355)
{
b=0;
}
else
{
}
return b;
}
float azimut (void) //vypocet aktualni vysky panelu
{
X= magR (MAG_XH, MAG_XL);
Y= magR (MAG_YH, MAG_YL);
Z= magR (MAG_ZH, MAG_ZL);
AX=abs(X);
AY=abs(Y);
AZ=abs(Z);
float a, b;
a=(float)Y/X;
b=atan(a);
b = (b/3.14)*180;
b=abs(b);
if(X==0) //osetreni proti deleni 0
{
if(Y>0)
{
b=90;
}
else
{
b=270;
}
}
else
{
if(X>0)
{
if(Y>=0)
{
b=b;
}
else
{
b=360-b;
}
}
else
{
if(Y>=0)
{
b=180-b;
}
else
{
b=180+b;
}
}
}
if(b>355)
{
b=0;
}
else
{
}
return b;
}
void motorA (int8 H) //pro ovladani prvniho motoru nastaveni vysky
{
switch(H){
case 1: //reverzní chod
output_low (AIN2);
output_high (AIN1);
break;
case 2: //dopøedu
output_low (AIN1);
output_high (AIN2);
break;
default:
output_low (AIN2);
output_low (AIN1);
}
}
void motorB (int8 H) //pro ovladani prvniho motoru nastaveni vysky
{
switch(H){
case 1: //reverzní chod
output_low (BIN2);
output_high (BIN1);
break;
case 2: //dopøedu
output_low (BIN1);
output_high (BIN2);
break;
default:
output_low (BIN2);
output_low (BIN1);
}
}
void elevace_set (int16 H) //slouzi pro nastaveni nove vysky panelu
{
//printf("Akcelerometr4: \r\n",);
float a;
int16 b,c;
a=elevace();
b= (int16) a;
c=abs(H-b);
while(c>2) //maximalni odchylka uhlu, aby nebylo potreba panelem hybat
{
while(H!=b) //probiha dokud se uhel panelu nerovna zadanemu na cele stupne
{
if(H>b)
{
motorA(2);
}
else
{
motorA(1);
}
delay_ms (50); //cas sepnuti motoru
motorA(3); //vypne motor
delay_ms (50); //doma na ustaleni panelu pred merenim
a=elevace();
b= (int16) a;
c=abs(H-b);
}
}
motorA(3); //vypne motor
printf("Podaøené nastavení výka: %Ld\r\n", b);
}
void azimut_set (int16 H) //slouzi pro nastaveni nove vysky panelu
{
float a;
int16 b,c;
a=azimut();
b= (int16) a;
c=abs(H-b);
while(c>2) //maximalni odchylka uhlu, aby nebylo potreba panelem hybat
{
while(H!=b) //probiha dokud se uhel panelu nerovna zadanemu na cele stupne
{
if(H>b)
{
motorB(2);
}
else
{
motorB(1);
}
delay_ms (50); //cas sepnuti motoru
motorB(3); //vypne motor
delay_ms (50); //doma na ustaleni panelu pred merenim
a=azimut();
b= (int16) a;
c=abs(H-b);
}
}
motorA(3); //vypne motor
printf("Podaøené nastavení azimut: %Ld\r\n", b);
}
void main()
{
setup_adc_ports(NO_ANALOGS|VSS_VDD);
setup_adc(ADC_CLOCK_DIV_2);
setup_spi(SPI_SS_DISABLED);
setup_timer_0(RTCC_INTERNAL|RTCC_DIV_1);
setup_timer_1(T1_DISABLED);
setup_timer_2(T2_DISABLED,0,1);
setup_ccp1(CCP_OFF);
setup_comparator(NC_NC_NC_NC);// This device COMP currently not supported by the PICWizard
setup_adc_ports(PIN_A0); //piny pro A/D RA0
setup_adc_ports(PIN_A1); //piny pro A/D RA1
motorA(3); //vyponuti motorù
motorB(3);
setAK(); //nastaveni akcelerometru
setmag();
printf("System nataceni panelu \r\n",);
while(TRUE)
{
int i[10];
int16 vysledek;
int b=0;
int c;
do {
b++;
i[b] = getchar();
// printf("zadaný azimut %d \r\n", i[b]);
} while (i[b] != ' ');
b=b-1;
switch(b){
case 1: //reverzní chod
elevaceZAD=i[1]-48;
break;
case 2: //dopøedu
elevaceZAD=(i[2]-48)+(i[1]-48)*10;
break;
case 3: //dopøedu
elevaceZAD=(i[3]-48)+(i[2]-48)*10+((int16)i[1]-48)*100;
break;
default:
}
printf("Zadaná elevace %Ld \r\n", elevaceZAD);
i=0;
vysledek=0;
b=0;
c=0;
do {
b++;
i[b] = getchar();
//printf("Zadaný azimut %d \r\n", i[b]);
} while (i[b] != ' ');
b=b-1;
switch(b){
case 1: //reverzní chod
azimutZAD=i[1]-48;
break;
case 2: //dopøedu
azimutZAD=(i[2]-48)+(i[1]-48)*10;
break;
case 3: //dopøedu
azimutZAD=(i[3]-48)+(i[2]-48)*10+((int16)i[1]-48)*100;
break;
default:
}
printf("Zadaný azimut %Ld \r\n", azimutZAD);
elevace_set (elevaceZAD);
azimut_set(azimutZAD);
delay_ms (2000);
}
}