ardupilot/ArduCopter/radio.pde

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// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
//Function that will read the radio data, limit servos and trigger a failsafe
// ----------------------------------------------------------------------------
static byte failsafeCounter = 0; // we wait a second to take over the throttle and send the plane circling
static void init_rc_in()
{
// set rc channel ranges
g.rc_1.set_angle(4500);
g.rc_2.set_angle(4500);
g.rc_3.set_range(0,1000);
g.rc_3.scale_output = .9;
g.rc_4.set_angle(4500);
// reverse: CW = left
// normal: CW = left???
g.rc_1.set_type(RC_CHANNEL_ANGLE_RAW);
g.rc_2.set_type(RC_CHANNEL_ANGLE_RAW);
g.rc_4.set_type(RC_CHANNEL_ANGLE_RAW);
// set rc dead zones
/*g.rc_1.dead_zone = 60;
g.rc_2.dead_zone = 60;
g.rc_3.dead_zone = 60;
g.rc_4.dead_zone = 300;
*/
g.rc_1.set_dead_zone(60);
g.rc_2.set_dead_zone(60);
g.rc_3.set_dead_zone(60);
2011-09-27 17:56:02 -03:00
g.rc_4.set_dead_zone(200);
//set auxiliary ranges
g.rc_5.set_range(0,1000);
g.rc_5.set_filter(false);
g.rc_6.set_range(0,1000);
g.rc_7.set_range(0,1000);
g.rc_8.set_range(0,1000);
}
static void init_rc_out()
{
#if ARM_AT_STARTUP == 1
motor_armed = 1;
#endif
APM_RC.Init(); // APM Radio initialization
// fix for crazy output
OCR1B = 0xFFFF; // PB6, OUT3
OCR1C = 0xFFFF; // PB7, OUT4
OCR5B = 0xFFFF; // PL4, OUT1
OCR5C = 0xFFFF; // PL5, OUT2
OCR4B = 0xFFFF; // PH4, OUT6
OCR4C = 0xFFFF; // PH5, OUT5
// this is the camera pitch5 and roll6
APM_RC.OutputCh(CH_5, 1500);
APM_RC.OutputCh(CH_6, 1500);
// don't fuss if we are calibrating
if(g.esc_calibrate == 1)
return;
if(g.rc_3.radio_min <= 1200){
output_min();
}
for(byte i = 0; i < 5; i++){
delay(20);
read_radio();
}
// sanity check
if(g.rc_3.radio_min >= 1300){
g.rc_3.radio_min = g.rc_3.radio_in;
output_min();
}
}
void output_min()
{
#if FRAME_CONFIG == HELI_FRAME
heli_move_servos_to_mid();
#else
APM_RC.OutputCh(CH_1, g.rc_3.radio_min); // Initialization of servo outputs
APM_RC.OutputCh(CH_2, g.rc_3.radio_min);
APM_RC.OutputCh(CH_3, g.rc_3.radio_min);
APM_RC.OutputCh(CH_4, g.rc_3.radio_min);
#endif
APM_RC.OutputCh(CH_7, g.rc_3.radio_min);
APM_RC.OutputCh(CH_8, g.rc_3.radio_min);
#if FRAME_CONFIG == OCTA_FRAME
APM_RC.OutputCh(CH_10, g.rc_3.radio_min);
APM_RC.OutputCh(CH_11, g.rc_3.radio_min);
#endif
}
static void read_radio()
{
if (APM_RC.GetState() == 1){
new_radio_frame = true;
g.rc_1.set_pwm(APM_RC.InputCh(CH_1));
g.rc_2.set_pwm(APM_RC.InputCh(CH_2));
g.rc_3.set_pwm(APM_RC.InputCh(CH_3));
g.rc_4.set_pwm(APM_RC.InputCh(CH_4));
g.rc_5.set_pwm(APM_RC.InputCh(CH_5));
g.rc_6.set_pwm(APM_RC.InputCh(CH_6));
g.rc_7.set_pwm(APM_RC.InputCh(CH_7));
g.rc_8.set_pwm(APM_RC.InputCh(CH_8));
#if FRAME_CONFIG != HELI_FRAME
// limit our input to 800 so we can still pitch and roll
g.rc_3.control_in = min(g.rc_3.control_in, 800);
#endif
//throttle_failsafe(g.rc_3.radio_in);
}
}
static void throttle_failsafe(uint16_t pwm)
{
if(g.throttle_fs_enabled == 0)
return;
//check for failsafe and debounce funky reads
// ------------------------------------------
if (pwm < (unsigned)g.throttle_fs_value){
// we detect a failsafe from radio
// throttle has dropped below the mark
failsafeCounter++;
if (failsafeCounter == 9){
SendDebug("MSG FS ON ");
SendDebugln(pwm, DEC);
}else if(failsafeCounter == 10) {
ch3_failsafe = true;
//set_failsafe(true);
//failsafeCounter = 10;
}else if (failsafeCounter > 10){
failsafeCounter = 11;
}
}else if(failsafeCounter > 0){
// we are no longer in failsafe condition
// but we need to recover quickly
failsafeCounter--;
if (failsafeCounter > 3){
failsafeCounter = 3;
}
if (failsafeCounter == 1){
SendDebug("MSG FS OFF ");
SendDebugln(pwm, DEC);
}else if(failsafeCounter == 0) {
ch3_failsafe = false;
//set_failsafe(false);
//failsafeCounter = -1;
}else if (failsafeCounter <0){
failsafeCounter = -1;
}
}
}
static void trim_radio()
{
for (byte i = 0; i < 30; i++){
read_radio();
}
g.rc_1.trim(); // roll
g.rc_2.trim(); // pitch
g.rc_4.trim(); // yaw
g.rc_1.save_eeprom();
g.rc_2.save_eeprom();
g.rc_4.save_eeprom();
}
static void trim_yaw()
{
for (byte i = 0; i < 30; i++){
read_radio();
}
g.rc_4.trim(); // yaw
}