int main(void)
{
DDRC |= 1<<LED2;
DDRC |= 1<<LED3;
init_TWI();
motor_init();
sei();
while(1)
{
if(new_cmd_flag){
process_cmd(cmd_buf);
}
}
}
int main(void)
{
DDRC = 0xff;
PORTC = 0x80;
uint8_t i;
char buf[10];
init_TWI();
while(1)
{
_delay_ms(1000);
get_HM_data();
if(hm.LoadStatus == 0xc8)
PORTC &= ~(0x80);
}
return 0;
}
int main(void){
//while(1);
wdt_disable();
///Configure the Torquer
configure_torquer();
char buf[100];
uint16_t v;
int ao;
for(ao=0;ao<1;ao++)
_delay_ms(1000);
/// Initialise Interfaces - UART of Magnetometer and GPS and the SPI bus
init_UART_MM();
init_UART_GPS();
init_SPI();
init_TWI();
send_preflight("Master\r", 7);
///Set Preflight pin as input
cbi(DDR_PF, PIN_PF);
///* Switch on Global interrupts
sei();
///Check if Preflight Pin is high
while(1){
///* * Reset timer for 2 seconds
timer_reset_two_sec();
//get_HM_data();
//send_preflight("Power\r", 6);
///* Preflight Checks
if(0){
///* * Set the mode as preflight
Mode = PREFLIGHT;
/*slave_send(HM_DATA, "Hello", 5);
_delay_ms(10);
slave_send (BEGIN_TX_GS, NULL, 0);
//power_up_peripheral(PCC);
_delay_ms(10);
ao = init_CC1020();
if(ao)
send_preflight("CC Init\r", 8);
else
send_preflight("No Init\r", 8);
while(1);*/
/*power_up_peripheral(PGPS);
while(1) {
read_GPS();
while(UCSR0B & _BV(RXCIE0));
copy_gps_reading();
sprintf(buf,"%ld %ld %ld\r", Current_state.gps.x/1000, Current_state.gps.y/1000, Current_state.gps.z/1000);
send_preflight(buf, strlen(buf));
sprintf(buf,"%ld %ld %ld\r", Current_state.gps.v_x/1000, Current_state.gps.v_y/1000, Current_state.gps.v_z/1000);
send_preflight(buf, strlen(buf));
_delay_ms(1000);
}*/
///* * Magnetometer and Torquer test
///* * Reading with one torquer on at once
/*Current_state.pwm.x_dir = 0;
Current_state.pwm.x = 10000;
Current_state.pwm.y_dir = 0;
Current_state.pwm.y = 30000;
Current_state.pwm.z_dir = 1;
Current_state.pwm.z = 20000;
send_preflight("Read\r", 5);
set_PWM();*/
while(1) {
read_SS();
//send_preflight((char *)&Current_state.ss, sizeof(struct SS_reading));
for(v = 0; v < 6; v++)
{
sprintf(buf,"%u\r", (uint16_t)(((float)Current_state.ss.reading[v])*1.6*100/4096));
send_preflight(buf, strlen(buf));
sprintf(buf,"%x\r", Current_state.ss.reading[v]);
send_preflight(buf, strlen(buf));
}
_delay_ms(1000);
}
///* * Set Torquer values to zero
reset_PWM();
while(1)
read_MM();
read_GPS();
send_preflight((char *)&Current_state.gps, sizeof(struct GPS_reading));
///* * Sunsensor test
read_SS();
send_preflight((char *)&Current_state.ss, sizeof(struct SS_reading));
///* Health Montoring
get_HM_data();
send_preflight((char *)&Current_state.hm, sizeof(struct HM_data));
///Communication Task
comm();
///* * Wait for 2 seconds to get over
timer_wait_reset();
}
///Normal Mode
else{
///* Set default mode of Satellite
Mode = DETUMBLING;
///* initialise Timer
Time = 0;
///Loop begins
while(1){
//Fuses Pain, Nominal Mode checking
send_preflight("Loop\r", 5);
control();
send_preflight("Control\r", 8);
//power();
comm();
send_preflight("Comm\r", 5);
v = StackCount();
sprintf(buf, "Stack = %d\r", v);
send_preflight(buf, strlen(buf));
v = get_free_memory();
sprintf(buf, "Stack(Method 2) = %d\r", v);
send_preflight(buf, strlen(buf));
Time += FRAME_TIME;
timer_wait_reset();
}
}
}
return 0;
}
int main(void){
///Configure the Torquer
configure_torquer();
_delay_ms(1000);
/// Initialise Interfaces - UART of Magnetometer and GPS and the SPI bus
init_UART_MM();
init_UART_GPS();
init_SPI();
init_TWI();
///Set Preflight pin as input
cbi(DDR_PF, PIN_PF);
///* Switch on Global interrupts
sei();
///Check if Preflight Pin is high
while(1){
///* * Reset timer for 2 seconds
timer_reset_two_sec();
///* Get Health Monitoring data
get_HM_data();
///* Preflight Checks
if(PORT_PF & _BV(PIN_PF)){
///* * Set the mode as preflight
Mode = PREFLIGHT;
send_preflight("Master\r", 7);
///* * GPS test
read_GPS();
while(UCSR0B & _BV(RXCIE0));
send_preflight((char *)&Current_state.gps, sizeof(struct GPS_reading));
///* * Magnetometer and Torquer test
///* * Reading with no torquers on
read_MM ();
send_preflight((char *)&Current_state.mm, sizeof(struct MM_reading));
///* * Reading with one torquer on at once
Current_state.pwm.x_dir = 0;
Current_state.pwm.x = 32768;
Current_state.pwm.y_dir = 0;
Current_state.pwm.y = 0;
Current_state.pwm.z_dir = 0;
Current_state.pwm.z = 0;
set_PWM ();
read_MM ();
send_preflight((char *)&Current_state.mm, sizeof(struct MM_reading));
Current_state.pwm.x_dir = 0;
Current_state.pwm.x = 0;
Current_state.pwm.y_dir = 0;
Current_state.pwm.y = 32768;
Current_state.pwm.z_dir = 0;
Current_state.pwm.z = 0;
set_PWM ();
read_MM ();
send_preflight((char *)&Current_state.mm, sizeof(struct MM_reading));
Current_state.pwm.x_dir = 0;
Current_state.pwm.x = 0;
Current_state.pwm.y_dir = 0;
Current_state.pwm.y = 0;
Current_state.pwm.z_dir = 0;
Current_state.pwm.z = 32768;
set_PWM ();
read_MM ();
send_preflight((char *)&Current_state.mm, sizeof(struct MM_reading));
///* * Reading with one torquer on at once, in other direction
Current_state.pwm.x_dir = 1;
Current_state.pwm.x = 32768;
Current_state.pwm.y_dir = 0;
Current_state.pwm.y = 0;
Current_state.pwm.z_dir = 0;
Current_state.pwm.z = 0;
set_PWM ();
read_MM ();
send_preflight((char *)&Current_state.mm, sizeof(struct MM_reading));
Current_state.pwm.x_dir = 0;
Current_state.pwm.x = 0;
Current_state.pwm.y_dir = 1;
Current_state.pwm.y = 32768;
Current_state.pwm.z_dir = 0;
Current_state.pwm.z = 0;
set_PWM ();
read_MM ();
send_preflight((char *)&Current_state.mm, sizeof(struct MM_reading));
Current_state.pwm.x_dir = 0;
Current_state.pwm.x = 0;
Current_state.pwm.y_dir = 0;
Current_state.pwm.y = 0;
Current_state.pwm.z_dir = 1;
Current_state.pwm.z = 32768;
set_PWM ();
read_MM ();
send_preflight((char *)&Current_state.mm, sizeof(struct MM_reading));
///* * Set Torquer values to zero
reset_PWM();
///* * Sunsensor test
read_SS();
send_preflight((char *)&Current_state.ss, sizeof(struct SS_reading));
///* Health Montoring
get_HM_data();
send_preflight((char *)&Current_state.hm, sizeof(struct HM_data));
///Communication Task
comm();
///* * Wait for 2 seconds to get over
timer_wait_reset();
}
///Normal Mode
else{
///* Set default mode of Satellite
Mode = DETUMBLING;
///* initialise Timer
Time = 0;
///Loop begins
while(!(PORT_PF & _BV(PIN_PF))){
/**
* * * * Task 2: Control codes
* @ref control
*/
control();
/**
* * * * Task 1: Communication with power uC through I2C. @ref power
*/
power();
/**
* * * * Task 3: Communication check routine;
* @ref comm
*/
comm();
wdt_disable();
///* * Increment the Timer
Time += FRAME_TIME;
///* * Wait for 2 seconds to get over
timer_wait_reset();
}
}
}
return 0;
}
