ardupilot/ArduCopterMega/radio.pde
jasonshort 73be185414 Big update 2.0.38
moved ground start to first arming
added ground start flag
moved throttle_integrator to 50hz loop
CAMERA_STABILIZER deprecated - now always on
renamed current logging bit mask to match APM
added MA filter to PID - D term
Adjusted PIDs based on continued testing and new PID filter
added MASK_LOG_SET_DEFAULTS to match APM
moved some stuff out of ground start into system start where it belonged
Added slower Yaw gains for DCM when the copter is in the air
changed camera output to be none scaled PWM
fixed bug where ground_temperature was unfiltered
shortened Baro startup time
fixed issue with Nav_WP integrator not being reset
RTL no longer yaws towards home
Circle mode for flying a 10m circle around the point where it was engaged. - Not tested at all! Consider Circle mode as alpha.


git-svn-id: https://arducopter.googlecode.com/svn/trunk@2966 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-30 20:42:54 +00:00

220 lines
5.1 KiB
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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; // 60 = .6 degrees
g.rc_2.dead_zone = 60;
g.rc_3.dead_zone = 60;
g.rc_4.dead_zone = 600;// 0 = hybrid rate approach
//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);
#if CHANNEL_6_TUNING == CH6_RATE_KP
g.rc_6.set_range(0,300); // 0 t0 .3
#elif CHANNEL_6_TUNING == CH6_RATE_KI
g.rc_6.set_range(0,300); // 0 t0 .3
#elif CHANNEL_6_TUNING == CH6_STABILIZE_KP
g.rc_6.set_range(0,8000); // 0 t0 .3
#elif CHANNEL_6_TUNING == CH6_STABILIZE_KI
g.rc_6.set_range(0,300); // 0 t0 .3
#elif CHANNEL_6_TUNING == CH6_THROTTLE_KP
g.rc_6.set_range(0,800); // 0 to .8
#elif CHANNEL_6_TUNING == CH6_THROTTLE_KD
g.rc_6.set_range(0,500); // 0 to .5
#elif CHANNEL_6_TUNING == CH6_TOP_BOTTOM_RATIO
g.rc_6.set_range(800,1000); // .8 to 1
/* #elif CHANNEL_6_TUNING == CH6_RELAY
g.rc_6.set_range(0,1000); // 0 to 1 */
#endif
}
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){
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);
/*
Serial.printf_P(PSTR("OUT 1: %d\t2: %d\t3: %d\t4: %d \n"),
g.rc_1.control_in,
g.rc_2.control_in,
g.rc_3.control_in,
g.rc_4.control_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
}