This commit is contained in:
Olivier ADLER 2011-09-11 18:36:54 +02:00
commit 226adc7cf1
42 changed files with 418 additions and 758 deletions

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@ -296,6 +296,7 @@ static boolean motor_auto_armed; // if true,
//int max_stabilize_dampener; //
//int max_yaw_dampener; //
static Vector3f omega;
float tuning_value;
// LED output
// ----------
@ -507,7 +508,7 @@ static byte simple_timer; // for limiting the execution of flight mode thi
static unsigned long dTnav; // Delta Time in milliseconds for navigation computations
static unsigned long nav_loopTimer; // used to track the elapsed ime for GPS nav
static float load; // % MCU cycles used
//static float load; // % MCU cycles used
static byte counter_one_herz;
static bool GPS_enabled = false;
@ -530,7 +531,7 @@ void loop()
//PORTK |= B00010000;
delta_ms_fast_loop = millis() - fast_loopTimer;
fast_loopTimer = millis();
load = float(fast_loopTimeStamp - fast_loopTimer) / delta_ms_fast_loop;
//load = float(fast_loopTimeStamp - fast_loopTimer) / delta_ms_fast_loop;
G_Dt = (float)delta_ms_fast_loop / 1000.f; // used by DCM integrator
mainLoop_count++;
@ -907,16 +908,15 @@ static void slow_loop()
// between 1 and 5 Hz
#else
gcs.send_message(MSG_LOCATION);
gcs.send_message(MSG_CPU_LOAD, load*100);
//gcs.send_message(MSG_CPU_LOAD, load*100);
#endif
#if HIL_PROTOCOL == HIL_PROTOCOL_MAVLINK && (HIL_MODE != HIL_MODE_DISABLED || HIL_PORT == 0)
hil.data_stream_send(1,5);
#endif
#if CHANNEL_6_TUNING != CH6_NONE
if(g.radio_tuning > 0)
tuning();
#endif
// filter out the baro offset.
//if(baro_alt_offset > 0) baro_alt_offset--;
@ -1301,7 +1301,7 @@ static void read_AHRS(void)
hil.update();
#endif
dcm.update_DCM(G_Dt);
dcm.update_DCM(G_Dt);//, _tog);
omega = dcm.get_gyro();
}
@ -1396,63 +1396,71 @@ adjust_altitude()
}
static void tuning(){
tuning_value = (float)g.rc_6.control_in / 1000.0;
//Outer Loop : Attitude
#if CHANNEL_6_TUNING == CH6_STABILIZE_KP
g.pi_stabilize_roll.kP((float)g.rc_6.control_in / 1000.0);
g.pi_stabilize_pitch.kP((float)g.rc_6.control_in / 1000.0);
switch(g.radio_tuning){
case CH6_STABILIZE_KP:
g.rc_6.set_range(0,8000); // 0 to 8
g.pi_stabilize_roll.kP(tuning_value);
g.pi_stabilize_pitch.kP(tuning_value);
break;
#elif CHANNEL_6_TUNING == CH6_STABILIZE_KI
g.pi_stabilize_roll.kI((float)g.rc_6.control_in / 1000.0);
g.pi_stabilize_pitch.kI((float)g.rc_6.control_in / 1000.0);
case CH6_STABILIZE_KI:
g.rc_6.set_range(0,300); // 0 to .3
tuning_value = (float)g.rc_6.control_in / 1000.0;
g.pi_stabilize_roll.kI(tuning_value);
g.pi_stabilize_pitch.kI(tuning_value);
break;
#elif CHANNEL_6_TUNING == CH6_YAW_KP
g.pi_stabilize_yaw.kP((float)g.rc_6.control_in / 1000.0); // range from 0.0 ~ 5.0
case CH6_RATE_KP:
g.rc_6.set_range(0,300); // 0 to .3
g.pi_rate_roll.kP(tuning_value);
g.pi_rate_pitch.kP(tuning_value);
break;
#elif CHANNEL_6_TUNING == CH6_YAW_KI
g.pi_stabilize_yaw.kI((float)g.rc_6.control_in / 1000.0);
case CH6_RATE_KI:
g.rc_6.set_range(0,300); // 0 to .3
g.pi_rate_roll.kI(tuning_value);
g.pi_rate_pitch.kI(tuning_value);
break;
case CH6_YAW_KP:
g.rc_6.set_range(0,1000);
g.pi_stabilize_yaw.kP(tuning_value);
break;
//Inner Loop : Rate
#elif CHANNEL_6_TUNING == CH6_RATE_KP
g.pi_rate_roll.kP((float)g.rc_6.control_in / 1000.0);
g.pi_rate_pitch.kP((float)g.rc_6.control_in / 1000.0);
case CH6_YAW_RATE_KP:
g.rc_6.set_range(0,1000);
g.pi_rate_yaw.kP(tuning_value);
break;
#elif CHANNEL_6_TUNING == CH6_RATE_KI
g.pi_rate_roll.kI((float)g.rc_6.control_in / 1000.0);
g.pi_rate_pitch.kI((float)g.rc_6.control_in / 1000.0);
case CH6_THROTTLE_KP:
g.rc_6.set_range(0,1000);
g.pi_throttle.kP(tuning_value);
break;
#elif CHANNEL_6_TUNING == CH6_YAW_RATE_KP
g.pi_rate_yaw.kP((float)g.rc_6.control_in / 1000.0);
case CH6_TOP_BOTTOM_RATIO:
g.rc_6.set_range(800,1000); // .8 to 1
g.top_bottom_ratio = tuning_value;
break;
#elif CHANNEL_6_TUNING == CH6_YAW_RATE_KI
g.pi_rate_yaw.kI((float)g.rc_6.control_in / 1000.0);
//Altitude Hold
#elif CHANNEL_6_TUNING == CH6_THROTTLE_KP
g.pi_throttle.kP((float)g.rc_6.control_in / 1000.0); // 0 to 1
#elif CHANNEL_6_TUNING == CH6_THROTTLE_KD
g.pi_throttle.kD((float)g.rc_6.control_in / 1000.0); // 0 to 1
//Extras
#elif CHANNEL_6_TUNING == CH6_TOP_BOTTOM_RATIO
g.top_bottom_ratio = (float)g.rc_6.control_in / 1000.0;
#elif CHANNEL_6_TUNING == CH6_TRAVERSE_SPEED
g.waypoint_speed_max = (float)g.rc_6.control_in / 1000.0;
#elif CHANNEL_6_TUNING == CH6_PMAX
g.pitch_max.set(g.rc_6.control_in * 2); // 0 to 2000
// Simple relay control
#elif CHANNEL_6_TUNING == CH6_RELAY
case CH6_RELAY:
g.rc_6.set_range(0,1000);
if (g.rc_6.control_in <= 600) relay_on();
if (g.rc_6.control_in >= 400) relay_off();
break;
#endif
case CH6_TRAVERSE_SPEED:
g.rc_6.set_range(0,1000);
g.waypoint_speed_max = g.rc_6.control_in;
break;
case CH6_NAV_P:
g.rc_6.set_range(0,6000);
g.pi_nav_lat.kP(tuning_value);
g.pi_nav_lon.kP(tuning_value);
break;
}
}
static void update_nav_wp()

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@ -102,7 +102,7 @@ get_nav_throttle(long z_error, int target_speed)
rate_error = constrain(rate_error, -110, 110);
throttle = g.pi_throttle.get_pi(rate_error, delta_ms_medium_loop);
return g.throttle_cruise + rate_error;
return g.throttle_cruise + throttle;
}

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@ -87,7 +87,7 @@ static bool mavlink_try_send_message(mavlink_channel_t chan, uint8_t id, uint16_
mode,
nav_mode,
status,
load * 1000,
0,
battery_voltage * 1000,
battery_remaining,
packet_drops);

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@ -77,6 +77,7 @@ public:
k_param_frame_orientation,
k_param_top_bottom_ratio,
k_param_optflow_enabled,
k_param_input_voltage,
//
// 160: Navigation parameters
@ -105,6 +106,7 @@ public:
k_param_throttle_fs_value,
k_param_throttle_cruise,
k_param_esc_calibrate,
k_param_radio_tuning,
#if FRAME_CONFIG == HELI_FRAME
@ -231,9 +233,12 @@ public:
AP_Int16 pack_capacity; // Battery pack capacity less reserve
AP_Int8 compass_enabled;
AP_Int8 esc_calibrate;
AP_Int8 radio_tuning;
AP_Int8 frame_orientation;
AP_Float top_bottom_ratio;
AP_Int8 optflow_enabled;
AP_Float input_voltage;
#if FRAME_CONFIG == HELI_FRAME
// Heli
@ -296,6 +301,7 @@ public:
pack_capacity (HIGH_DISCHARGE, k_param_pack_capacity, PSTR("BATT_CAPACITY")),
compass_enabled (MAGNETOMETER, k_param_compass_enabled, PSTR("MAG_ENABLE")),
optflow_enabled (OPTFLOW, k_param_optflow_enabled, PSTR("FLOW_ENABLE")),
input_voltage (INPUT_VOLTAGE, k_param_input_voltage, PSTR("IN_VOLT")),
waypoint_mode (0, k_param_waypoint_mode, PSTR("WP_MODE")),
waypoint_total (0, k_param_waypoint_total, PSTR("WP_TOTAL")),
@ -324,6 +330,7 @@ public:
log_bitmask (DEFAULT_LOG_BITMASK, k_param_log_bitmask, PSTR("LOG_BITMASK")),
RTL_altitude (ALT_HOLD_HOME * 100, k_param_RTL_altitude, PSTR("ALT_HOLD_RTL")),
esc_calibrate (0, k_param_esc_calibrate, PSTR("ESC")),
radio_tuning (0, k_param_radio_tuning, PSTR("TUNE")),
frame_orientation (FRAME_ORIENTATION, k_param_frame_orientation, PSTR("FRAME")),
top_bottom_ratio (TOP_BOTTOM_RATIO, k_param_top_bottom_ratio, PSTR("TB_RATIO")),

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@ -513,7 +513,7 @@
// Throttle control gains
//
#ifndef THROTTLE_P
# define THROTTLE_P 0.35 //
# define THROTTLE_P 0.6 //
#endif
#ifndef THROTTLE_I
# define THROTTLE_I 0.10 // with 4m error, 12.5s windup
@ -522,7 +522,7 @@
//# define THROTTLE_D 0.6 // upped with filter
//#endif
#ifndef THROTTLE_IMAX
# define THROTTLE_IMAX 150
# define THROTTLE_IMAX 300
#endif

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@ -138,13 +138,6 @@
#define CIRCLE 8 // AUTO control
#define NUM_MODES 9
// YAW debug
// ---------
#define YAW_HOLD 0
#define YAW_BRAKE 1
#define YAW_RATE 2
// CH_6 Tuning
// -----------
#define CH6_NONE 0
@ -152,20 +145,18 @@
#define CH6_STABILIZE_KP 1
#define CH6_STABILIZE_KI 2
#define CH6_YAW_KP 3
#define CH6_YAW_KD 4
// Rate
#define CH6_RATE_KP 5
#define CH6_RATE_KI 6
#define CH6_YAW_RATE_KP 7
#define CH6_YAW_RATE_KD 8
#define CH6_RATE_KP 4
#define CH6_RATE_KI 5
#define CH6_YAW_RATE_KP 6
// Altitude
#define CH6_THROTTLE_KP 9
#define CH6_THROTTLE_KD 10
#define CH6_THROTTLE_KP 7
// Extras
#define CH6_TOP_BOTTOM_RATIO 11
#define CH6_PMAX 12
#define CH6_RELAY 13
#define CH6_TRAVERSE_SPEED 14
#define CH6_TOP_BOTTOM_RATIO 8
#define CH6_RELAY 9
#define CH6_TRAVERSE_SPEED 10
#define CH6_NAV_P 11
// nav byte mask
// -------------
@ -322,8 +313,8 @@
#define ALTITUDE_HISTORY_LENGTH 8 //Number of (time,altitude) points to regress a climb rate from
#define BATTERY_VOLTAGE(x) (x*(INPUT_VOLTAGE/1024.0))*VOLT_DIV_RATIO
#define CURRENT_AMPS(x) ((x*(INPUT_VOLTAGE/1024.0))-CURR_AMPS_OFFSET)*CURR_AMP_PER_VOLT
#define BATTERY_VOLTAGE(x) (x*(g.input_voltage/1024.0))*VOLT_DIV_RATIO
#define CURRENT_AMPS(x) ((x*(g.input_voltage/1024.0))-CURR_AMPS_OFFSET)*CURR_AMP_PER_VOLT
//#define BARO_FILTER_SIZE 8
/* ************************************************************** */

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@ -35,30 +35,6 @@ static void init_rc_in()
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()

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@ -13,6 +13,7 @@ static int8_t setup_flightmodes (uint8_t argc, const Menu::arg *argv);
static int8_t setup_batt_monitor (uint8_t argc, const Menu::arg *argv);
static int8_t setup_sonar (uint8_t argc, const Menu::arg *argv);
static int8_t setup_compass (uint8_t argc, const Menu::arg *argv);
static int8_t setup_tune (uint8_t argc, const Menu::arg *argv);
//static int8_t setup_mag_offset (uint8_t argc, const Menu::arg *argv);
static int8_t setup_declination (uint8_t argc, const Menu::arg *argv);
static int8_t setup_esc (uint8_t argc, const Menu::arg *argv);
@ -41,6 +42,7 @@ const struct Menu::command setup_menu_commands[] PROGMEM = {
{"battery", setup_batt_monitor},
{"sonar", setup_sonar},
{"compass", setup_compass},
{"tune", setup_tune},
// {"offsets", setup_mag_offset},
{"declination", setup_declination},
#ifdef OPTFLOW_ENABLED
@ -354,6 +356,15 @@ setup_declination(uint8_t argc, const Menu::arg *argv)
return 0;
}
static int8_t
setup_tune(uint8_t argc, const Menu::arg *argv)
{
g.radio_tuning.set_and_save(argv[1].i);
report_tuning();
return 0;
}
static int8_t
setup_erase(uint8_t argc, const Menu::arg *argv)
@ -1131,3 +1142,15 @@ static void report_version()
print_blanks(2);
}
static void report_tuning()
{
Serial.printf_P(PSTR("\nTUNE:\n"));
print_divider();
if (g.radio_tuning == 0){
print_enabled(g.radio_tuning.get());
}else{
Serial.printf_P(PSTR(" %d\n"),(int)g.radio_tuning.get());
}
print_blanks(2);
}

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@ -41,7 +41,7 @@ const struct Menu::command main_menu_commands[] PROGMEM = {
};
// Create the top-level menu object.
MENU(main_menu, "ArduCopter 2.0.40 Beta", main_menu_commands);
MENU(main_menu, "ArduCopter 2.0.41 Beta", main_menu_commands);
#endif // CLI_ENABLED

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@ -636,59 +636,8 @@ test_tuning(uint8_t argc, const Menu::arg *argv)
while(1){
delay(200);
read_radio();
//Outer Loop : Attitude
#if CHANNEL_6_TUNING == CH6_NONE
Serial.printf_P(PSTR("disabled\n"));
#elif CHANNEL_6_TUNING == CH6_STABILIZE_KP
Serial.printf_P(PSTR("stab kP: %1.3f\n"), ((float)g.rc_6.control_in / 1000.0));
#elif CHANNEL_6_TUNING == CH6_STABILIZE_KI
Serial.printf_P(PSTR("stab kI: %1.3f\n"), ((float)g.rc_6.control_in / 1000.0));
#elif CHANNEL_6_TUNING == CH6_YAW_KP
Serial.printf_P(PSTR("yaw Hold kP: %1.3f\n"), ((float)g.rc_6.control_in / 1000.0)); // range from 0 ~ 5.0
#elif CHANNEL_6_TUNING == CH6_YAW_KI
Serial.printf_P(PSTR("yaw Hold kI: %1.3f\n"), ((float)g.rc_6.control_in / 1000.0));
//Inner Loop : Rate
#elif CHANNEL_6_TUNING == CH6_RATE_KP
Serial.printf_P(PSTR("rate kD: %1.3f\n"), ((float)g.rc_6.control_in / 1000.0));
#elif CHANNEL_6_TUNING == CH6_RATE_KI
Serial.printf_P(PSTR("rate kI: %1.3f\n"), ((float)g.rc_6.control_in / 1000.0));
#elif CHANNEL_6_TUNING == CH6_YAW_RATE_KP
Serial.printf_P(PSTR("yaw rate kP: %1.3f\n"), ((float)g.rc_6.control_in / 1000.0));
#elif CHANNEL_6_TUNING == CH6_YAW_RATE_KI
Serial.printf_P(PSTR("yaw rate kI: %1.3f\n"), ((float)g.rc_6.control_in / 1000.0));
//Altitude Hold
#elif CHANNEL_6_TUNING == CH6_THROTTLE_KP
Serial.printf_P(PSTR("throttle kP: %1.3f\n"), ((float)g.rc_6.control_in / 1000.0));
#elif CHANNEL_6_TUNING == CH6_THROTTLE_KD
Serial.printf_P(PSTR("baro kD: %1.3f\n"), ((float)g.rc_6.control_in / 1000.0));
#elif CHANNEL_6_TUNING == CH6_TRAVERSE_SPEED
Serial.printf_P(PSTR("traverse: %1.3f\n"), ((float)g.rc_6.control_in / 1000.0));
//Extras
#elif CHANNEL_6_TUNING == CH6_TOP_BOTTOM_RATIO
Serial.printf_P(PSTR("Y6: %1.3f\n"), ((float)g.rc_6.control_in / 1000.0));
#elif CHANNEL_6_TUNING == CH6_PMAX
Serial.printf_P(PSTR("Y6: %d\n"), (g.rc_6.control_in * 2));
#elif CHANNEL_6_TUNING == CH6_RELAY
Serial.printf_P(PSTR(" %d\n"), (g.rc_6.control_in ));
#endif
tuning();
Serial.printf_P(PSTR("tune: %1.3f\n"), tuning_value);
if(Serial.available() > 0){
return (0);
@ -1009,10 +958,12 @@ test_mission(uint8_t argc, const Menu::arg *argv)
return (0);
}
*/
static void print_hit_enter()
{
Serial.printf_P(PSTR("Hit Enter to exit.\n\n"));
}
/*
static void fake_out_gps()
{

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@ -131,7 +131,8 @@ GCS_MAVLINK::data_stream_send(uint16_t freqMin, uint16_t freqMax)
}
if (freqLoopMatch(streamRateExtra3, freqMin, freqMax)){
send_message(MSG_RAW_ADC);
// Available datastream
//Serial.printf("mav8 %d\n", (int)streamRateExtra3.get());
}
}
}

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@ -344,20 +344,6 @@ static bool mavlink_try_send_message(mavlink_channel_t chan, uint8_t id, uint16_
break;
}
case MSG_RAW_ADC:
{
CHECK_PAYLOAD_SIZE(AP_ADC);
mavlink_msg_ap_adc_send(chan,
analogRead(BATTERY_PIN1),
analogRead(BATTERY_PIN2),
analogRead(BATTERY_PIN3),
analogRead(BATTERY_PIN4),
analogRead(AN4),
analogRead(AN5));
break;
}
default:
break;
}
@ -365,7 +351,7 @@ static bool mavlink_try_send_message(mavlink_channel_t chan, uint8_t id, uint16_
}
#define MAX_DEFERRED_MESSAGES 18 // should be at least equal to number of
#define MAX_DEFERRED_MESSAGES 17 // should be at least equal to number of
// switch types in mavlink_try_send_message()
static struct mavlink_queue {
uint8_t deferred_messages[MAX_DEFERRED_MESSAGES];

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@ -176,7 +176,6 @@
#define MSG_GPS_RAW 0x64
#define MSG_SERVO_OUT 0x70
#define MSG_RAW_ADC 0x71
#define MSG_PIN_REQUEST 0x80
#define MSG_PIN_SET 0x81

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@ -3,7 +3,6 @@
In file included from /root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:53:
/usr/local/share/arduino/libraries/SPI/SPI.h:25:1: warning: "SPI_CLOCK_DIV64" redefined
/usr/local/share/arduino/libraries/SPI/SPI.h:20:1: warning: this is the location of the previous definition
/root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:1398: warning: 'void tuning()' defined but not used
autogenerated:34: warning: 'int alt_hold_velocity()' declared 'static' but never defined
autogenerated:86: warning: 'void acknowledge(byte, byte, byte)' declared 'static' but never defined
autogenerated:87: warning: 'void send_message(byte)' declared 'static' but never defined
@ -31,8 +30,8 @@ autogenerated:250: warning: 'void calc_altitude_smoothing_error()' declared 'sta
/root/apm/ardupilot-mega/ArduCopter/navigation.pde:217: warning: 'void reset_crosstrack()' defined but not used
/root/apm/ardupilot-mega/ArduCopter/navigation.pde:222: warning: 'long int get_altitude_above_home()' defined but not used
/root/apm/ardupilot-mega/ArduCopter/navigation.pde:243: warning: 'long int get_alt_distance(Location*, Location*)' defined but not used
/root/apm/ardupilot-mega/ArduCopter/radio.pde:155: warning: 'void throttle_failsafe(uint16_t)' defined but not used
/root/apm/ardupilot-mega/ArduCopter/radio.pde:212: warning: 'void trim_yaw()' defined but not used
/root/apm/ardupilot-mega/ArduCopter/radio.pde:131: warning: 'void throttle_failsafe(uint16_t)' defined but not used
/root/apm/ardupilot-mega/ArduCopter/radio.pde:188: warning: 'void trim_yaw()' defined but not used
autogenerated:268: warning: 'void readCommands()' declared 'static' but never defined
autogenerated:269: warning: 'void parseCommand(char*)' declared 'static' but never defined
/root/apm/ardupilot-mega/ArduCopter/sensors.pde:6: warning: 'void ReadSCP1000()' defined but not used
@ -44,14 +43,14 @@ autogenerated:287: warning: 'void report_gyro()' declared 'static' but never def
autogenerated:295: warning: 'RC_Channel* heli_get_servo(int)' declared 'static' but never defined
autogenerated:296: warning: 'int read_num_from_serial()' declared 'static' but never defined
/root/apm/ardupilot-mega/ArduCopter/system.pde:465: warning: 'void set_failsafe(boolean)' defined but not used
autogenerated:310: warning: 'void init_optflow()' declared 'static' but never defined
autogenerated:318: warning: 'void fake_out_gps()' declared 'static' but never defined
/root/apm/ardupilot-mega/ArduCopter/test.pde:1040: warning: 'void print_motor_out()' defined but not used
/root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:442: warning: 'undo_event' defined but not used
/root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:448: warning: 'condition_rate' defined but not used
/root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:462: warning: 'simple_WP' defined but not used
/root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:467: warning: 'optflow_offset' defined but not used
/root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:468: warning: 'new_location' defined but not used
autogenerated:311: warning: 'void init_optflow()' declared 'static' but never defined
autogenerated:319: warning: 'void fake_out_gps()' declared 'static' but never defined
/root/apm/ardupilot-mega/ArduCopter/test.pde:991: warning: 'void print_motor_out()' defined but not used
/root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:443: warning: 'undo_event' defined but not used
/root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:449: warning: 'condition_rate' defined but not used
/root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:463: warning: 'simple_WP' defined but not used
/root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:468: warning: 'optflow_offset' defined but not used
/root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:469: warning: 'new_location' defined but not used
%% libraries/APM_BMP085/APM_BMP085.o
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%% libraries/APM_RC/APM_RC.o

View File

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In file included from /root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:53:
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%% libraries/APM_BMP085/APM_BMP085.o
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%% libraries/APM_RC/APM_RC.o

View File

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View File

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In file included from /root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:53:
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%% libraries/APM_BMP085/APM_BMP085.o

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In file included from /root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:53:
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%% libraries/APM_BMP085/APM_BMP085.o

View File

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In file included from /root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:53:
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%% libraries/APM_BMP085/APM_BMP085.o
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%% libraries/APM_RC/APM_RC.o

View File

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View File

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In file included from /root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:53:
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%% libraries/APM_BMP085/APM_BMP085.o
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%% libraries/APM_RC/APM_RC.o

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In file included from /root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:53:
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%% libraries/APM_BMP085/APM_BMP085.o
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%% libraries/APM_RC/APM_RC.o

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In file included from /root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:53:
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%% libraries/APM_BMP085/APM_BMP085.o
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%% libraries/APM_RC/APM_RC.o

View File

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In file included from /root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:53:
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%% libraries/APM_BMP085/APM_BMP085.o
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%% libraries/APM_RC/APM_RC.o

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In file included from /root/apm/ardupilot-mega/ArduCopter/ArduCopter.pde:53:
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%% libraries/APM_BMP085/APM_BMP085.o
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%% libraries/APM_RC/APM_RC.o

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00000092 t test_tuning(unsigned char, Menu::arg const*)
00000095 r init_ardupilot()::__c
00000096 t map_baudrate(signed char, unsigned long)
00000096 t print_wp(Location*, unsigned char)
@ -549,12 +555,12 @@
000000ca t init_barometer()
000000cc t read_radio()
000000d0 t get_bearing(Location*, Location*)
000000d0 r setup_menu_commands
000000d8 t test_radio(unsigned char, Menu::arg const*)
000000d8 t read_barometer()
000000dc t test_adc(unsigned char, Menu::arg const*)
000000de t Log_Read_Performance()
000000de t Log_Read_Control_Tuning()
000000e0 r setup_menu_commands
000000e0 b mavlink_parse_char::m_mavlink_message
000000e4 t test_radio_pwm(unsigned char, Menu::arg const*)
000000e4 t Log_Read_Optflow()
@ -595,18 +601,19 @@
0000021c t test_wp(unsigned char, Menu::arg const*)
00000228 t setup_radio(unsigned char, Menu::arg const*)
00000286 t test_imu(unsigned char, Menu::arg const*)
0000031e t read_battery()
000002ea t tuning()
00000330 t calc_nav_rate(int, int, int, int)
00000358 T update_throttle_mode()
00000382 t print_log_menu()
000003be t read_battery()
000003dc T update_yaw_mode()
000004b2 t mavlink_parse_char
000005ea T update_roll_pitch_mode()
0000062e t init_ardupilot()
00000798 t __static_initialization_and_destruction_0(int, int)
000007c1 b g
000007d6 W Parameters::Parameters()
000007a8 t __static_initialization_and_destruction_0(int, int)
000007dc b g
0000083c W Parameters::Parameters()
000008e4 t process_next_command()
000011d8 T GCS_MAVLINK::handleMessage(__mavlink_message*)
000017d0 t mavlink_try_send_message(mavlink_channel_t, unsigned char, unsigned int)
00001f0c T loop
000017ac t mavlink_try_send_message(mavlink_channel_t, unsigned char, unsigned int)
00001ec4 T loop

View File

@ -58,7 +58,7 @@
<Firmware>
<url>http://ardupilot-mega.googlecode.com/git/Tools/ArdupilotMegaPlanner/Firmware/AC2-Quad-1280.hex</url>
<url2560>http://ardupilot-mega.googlecode.com/git/Tools/ArdupilotMegaPlanner/Firmware/AC2-Quad-2560.hex</url2560>
<name>ArduCopter 2.0.40 Beta Quad</name>
<name>ArduCopter 2.0.41 Beta Quad</name>
<desc>
#define FRAME_CONFIG QUAD_FRAME
#define FRAME_ORIENTATION X_FRAME
@ -69,7 +69,7 @@
<Firmware>
<url>http://ardupilot-mega.googlecode.com/git/Tools/ArdupilotMegaPlanner/Firmware/AC2-Tri-1280.hex</url>
<url2560>http://ardupilot-mega.googlecode.com/git/Tools/ArdupilotMegaPlanner/Firmware/AC2-Tri-2560.hex</url2560>
<name>ArduCopter 2.0.40 Beta Tri</name>
<name>ArduCopter 2.0.41 Beta Tri</name>
<desc>
#define FRAME_CONFIG TRI_FRAME
#define FRAME_ORIENTATION X_FRAME
@ -80,7 +80,7 @@
<Firmware>
<url>http://ardupilot-mega.googlecode.com/git/Tools/ArdupilotMegaPlanner/Firmware/AC2-Hexa-1280.hex</url>
<url2560>http://ardupilot-mega.googlecode.com/git/Tools/ArdupilotMegaPlanner/Firmware/AC2-Hexa-2560.hex</url2560>
<name>ArduCopter 2.0.40 Beta Hexa</name>
<name>ArduCopter 2.0.41 Beta Hexa</name>
<desc>
#define FRAME_CONFIG HEXA_FRAME
#define FRAME_ORIENTATION X_FRAME
@ -91,7 +91,7 @@
<Firmware>
<url>http://ardupilot-mega.googlecode.com/git/Tools/ArdupilotMegaPlanner/Firmware/AC2-Y6-1280.hex</url>
<url2560>http://ardupilot-mega.googlecode.com/git/Tools/ArdupilotMegaPlanner/Firmware/AC2-Y6-2560.hex</url2560>
<name>ArduCopter 2.0.40 Beta Y6</name>
<name>ArduCopter 2.0.41 Beta Y6</name>
<desc>
#define FRAME_CONFIG Y6_FRAME
#define FRAME_ORIENTATION X_FRAME
@ -102,7 +102,7 @@
<Firmware>
<url>http://ardupilot-mega.googlecode.com/git/Tools/ArdupilotMegaPlanner/Firmware/AC2-Heli-1280.hex</url>
<url2560>http://ardupilot-mega.googlecode.com/git/Tools/ArdupilotMegaPlanner/Firmware/AC2-Heli-2560.hex</url2560>
<name>ArduCopter 2.0.40 Beta Heli (2560 only)</name>
<name>ArduCopter 2.0.41 Beta Heli (2560 only)</name>
<desc>
#define AUTO_RESET_LOITER 0
#define FRAME_CONFIG HELI_FRAME
@ -149,7 +149,7 @@
<Firmware>
<url>http://ardupilot-mega.googlecode.com/git/Tools/ArdupilotMegaPlanner/Firmware/AC2-QUADHIL-1280.hex</url>
<url2560>http://ardupilot-mega.googlecode.com/git/Tools/ArdupilotMegaPlanner/Firmware/AC2-QUADHIL-2560.hex</url2560>
<name>ArduCopter 2.0.40 Beta Quad Hil</name>
<name>ArduCopter 2.0.41 Beta Quad Hil</name>
<desc>
#define FRAME_CONFIG QUAD_FRAME
#define FRAME_ORIENTATION PLUS_FRAME

View File

@ -1 +1,9 @@
Already up-to-date.
From https://code.google.com/p/ardupilot-mega
22593cc..5e95582 APM_Camera -> origin/APM_Camera
0448983..dc0031c master -> origin/master
Updating 0448983..dc0031c
Fast-forward
ArduCopter/ArduCopter.pde | 6 ++++++
ArduCopter/Parameters.h | 3 +++
ArduCopter/defines.h | 6 ++++--
3 files changed, 13 insertions(+), 2 deletions(-)

View File

@ -12,15 +12,15 @@ extern "C" {
// MESSAGE LENGTHS AND CRCS
#ifndef MAVLINK_MESSAGE_LENGTHS
#define MAVLINK_MESSAGE_LENGTHS {3, 4, 8, 14, 8, 28, 3, 32, 0, 2, 3, 2, 2, 0, 0, 0, 0, 0, 0, 0, 19, 2, 23, 21, 0, 37, 26, 101, 26, 16, 32, 32, 37, 32, 11, 17, 17, 16, 18, 36, 4, 4, 2, 2, 4, 2, 2, 3, 14, 12, 18, 16, 8, 27, 25, 18, 18, 24, 24, 0, 0, 0, 26, 16, 36, 5, 6, 56, 26, 21, 18, 0, 0, 18, 20, 20, 8, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 18, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 36, 0, 0, 0, 0, 0, 0, 0, 0, 0, 42, 8, 4, 12, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 30, 14, 14, 51, 5}
#define MAVLINK_MESSAGE_LENGTHS {3, 4, 8, 14, 8, 28, 3, 32, 0, 2, 3, 2, 2, 0, 0, 0, 0, 0, 0, 0, 19, 2, 23, 21, 0, 37, 26, 101, 26, 16, 32, 32, 37, 32, 11, 17, 17, 16, 18, 36, 4, 4, 2, 2, 4, 2, 2, 3, 14, 12, 18, 16, 8, 27, 25, 18, 18, 24, 24, 0, 0, 0, 26, 16, 36, 5, 6, 56, 26, 21, 18, 0, 0, 18, 20, 20, 8, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 18, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 36, 0, 0, 0, 0, 0, 0, 0, 0, 0, 42, 8, 4, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 30, 14, 14, 51, 5}
#endif
#ifndef MAVLINK_MESSAGE_CRCS
#define MAVLINK_MESSAGE_CRCS {72, 39, 190, 92, 191, 217, 104, 119, 0, 219, 60, 186, 10, 0, 0, 0, 0, 0, 0, 0, 89, 159, 162, 121, 0, 149, 222, 110, 179, 136, 66, 126, 185, 147, 112, 252, 162, 215, 229, 128, 9, 106, 101, 213, 4, 229, 21, 214, 215, 14, 206, 50, 157, 126, 108, 213, 95, 5, 127, 0, 0, 0, 57, 126, 130, 119, 193, 191, 236, 158, 143, 0, 0, 104, 123, 131, 8, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 174, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 155, 0, 0, 0, 0, 0, 0, 0, 0, 0, 143, 29, 208, 188, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 178, 224, 60, 106, 7}
#define MAVLINK_MESSAGE_CRCS {72, 39, 190, 92, 191, 217, 104, 119, 0, 219, 60, 186, 10, 0, 0, 0, 0, 0, 0, 0, 89, 159, 162, 121, 0, 149, 222, 110, 179, 136, 66, 126, 185, 147, 112, 252, 162, 215, 229, 128, 9, 106, 101, 213, 4, 229, 21, 214, 215, 14, 206, 50, 157, 126, 108, 213, 95, 5, 127, 0, 0, 0, 57, 126, 130, 119, 193, 191, 236, 158, 143, 0, 0, 104, 123, 131, 8, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 174, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 155, 0, 0, 0, 0, 0, 0, 0, 0, 0, 143, 29, 208, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 178, 224, 60, 106, 7}
#endif
#ifndef MAVLINK_MESSAGE_INFO
#define MAVLINK_MESSAGE_INFO {MAVLINK_MESSAGE_INFO_HEARTBEAT, MAVLINK_MESSAGE_INFO_BOOT, MAVLINK_MESSAGE_INFO_SYSTEM_TIME, MAVLINK_MESSAGE_INFO_PING, MAVLINK_MESSAGE_INFO_SYSTEM_TIME_UTC, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL_ACK, MAVLINK_MESSAGE_INFO_AUTH_KEY, {NULL}, MAVLINK_MESSAGE_INFO_ACTION_ACK, MAVLINK_MESSAGE_INFO_ACTION, MAVLINK_MESSAGE_INFO_SET_MODE, MAVLINK_MESSAGE_INFO_SET_NAV_MODE, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_READ, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_LIST, MAVLINK_MESSAGE_INFO_PARAM_VALUE, MAVLINK_MESSAGE_INFO_PARAM_SET, {NULL}, MAVLINK_MESSAGE_INFO_GPS_RAW_INT, MAVLINK_MESSAGE_INFO_SCALED_IMU, MAVLINK_MESSAGE_INFO_GPS_STATUS, MAVLINK_MESSAGE_INFO_RAW_IMU, MAVLINK_MESSAGE_INFO_RAW_PRESSURE, MAVLINK_MESSAGE_INFO_ATTITUDE, MAVLINK_MESSAGE_INFO_LOCAL_POSITION, MAVLINK_MESSAGE_INFO_GPS_RAW, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION, MAVLINK_MESSAGE_INFO_SYS_STATUS, MAVLINK_MESSAGE_INFO_RC_CHANNELS_RAW, MAVLINK_MESSAGE_INFO_RC_CHANNELS_SCALED, MAVLINK_MESSAGE_INFO_SERVO_OUTPUT_RAW, MAVLINK_MESSAGE_INFO_SCALED_PRESSURE, MAVLINK_MESSAGE_INFO_WAYPOINT, MAVLINK_MESSAGE_INFO_WAYPOINT_REQUEST, MAVLINK_MESSAGE_INFO_WAYPOINT_SET_CURRENT, MAVLINK_MESSAGE_INFO_WAYPOINT_CURRENT, MAVLINK_MESSAGE_INFO_WAYPOINT_REQUEST_LIST, MAVLINK_MESSAGE_INFO_WAYPOINT_COUNT, MAVLINK_MESSAGE_INFO_WAYPOINT_CLEAR_ALL, MAVLINK_MESSAGE_INFO_WAYPOINT_REACHED, MAVLINK_MESSAGE_INFO_WAYPOINT_ACK, MAVLINK_MESSAGE_INFO_GPS_SET_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_GPS_LOCAL_ORIGIN_SET, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_SETPOINT_SET, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_CONTROL_STATUS, MAVLINK_MESSAGE_INFO_SAFETY_SET_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SAFETY_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_SPEED_THRUST, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, {NULL}, {NULL}, {NULL}, MAVLINK_MESSAGE_INFO_NAV_CONTROLLER_OUTPUT, MAVLINK_MESSAGE_INFO_POSITION_TARGET, MAVLINK_MESSAGE_INFO_STATE_CORRECTION, MAVLINK_MESSAGE_INFO_SET_ALTITUDE, MAVLINK_MESSAGE_INFO_REQUEST_DATA_STREAM, MAVLINK_MESSAGE_INFO_HIL_STATE, MAVLINK_MESSAGE_INFO_HIL_CONTROLS, MAVLINK_MESSAGE_INFO_MANUAL_CONTROL, MAVLINK_MESSAGE_INFO_RC_CHANNELS_OVERRIDE, {NULL}, {NULL}, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_INT, MAVLINK_MESSAGE_INFO_VFR_HUD, MAVLINK_MESSAGE_INFO_COMMAND, MAVLINK_MESSAGE_INFO_COMMAND_ACK, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, MAVLINK_MESSAGE_INFO_OPTICAL_FLOW, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, MAVLINK_MESSAGE_INFO_OBJECT_DETECTION_EVENT, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, MAVLINK_MESSAGE_INFO_SENSOR_OFFSETS, MAVLINK_MESSAGE_INFO_SET_MAG_OFFSETS, MAVLINK_MESSAGE_INFO_MEMINFO, MAVLINK_MESSAGE_INFO_AP_ADC, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, MAVLINK_MESSAGE_INFO_DEBUG_VECT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_FLOAT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_INT, MAVLINK_MESSAGE_INFO_STATUSTEXT, MAVLINK_MESSAGE_INFO_DEBUG}
#define MAVLINK_MESSAGE_INFO {MAVLINK_MESSAGE_INFO_HEARTBEAT, MAVLINK_MESSAGE_INFO_BOOT, MAVLINK_MESSAGE_INFO_SYSTEM_TIME, MAVLINK_MESSAGE_INFO_PING, MAVLINK_MESSAGE_INFO_SYSTEM_TIME_UTC, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL, MAVLINK_MESSAGE_INFO_CHANGE_OPERATOR_CONTROL_ACK, MAVLINK_MESSAGE_INFO_AUTH_KEY, {NULL}, MAVLINK_MESSAGE_INFO_ACTION_ACK, MAVLINK_MESSAGE_INFO_ACTION, MAVLINK_MESSAGE_INFO_SET_MODE, MAVLINK_MESSAGE_INFO_SET_NAV_MODE, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_READ, MAVLINK_MESSAGE_INFO_PARAM_REQUEST_LIST, MAVLINK_MESSAGE_INFO_PARAM_VALUE, MAVLINK_MESSAGE_INFO_PARAM_SET, {NULL}, MAVLINK_MESSAGE_INFO_GPS_RAW_INT, MAVLINK_MESSAGE_INFO_SCALED_IMU, MAVLINK_MESSAGE_INFO_GPS_STATUS, MAVLINK_MESSAGE_INFO_RAW_IMU, MAVLINK_MESSAGE_INFO_RAW_PRESSURE, MAVLINK_MESSAGE_INFO_ATTITUDE, MAVLINK_MESSAGE_INFO_LOCAL_POSITION, MAVLINK_MESSAGE_INFO_GPS_RAW, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION, MAVLINK_MESSAGE_INFO_SYS_STATUS, MAVLINK_MESSAGE_INFO_RC_CHANNELS_RAW, MAVLINK_MESSAGE_INFO_RC_CHANNELS_SCALED, MAVLINK_MESSAGE_INFO_SERVO_OUTPUT_RAW, MAVLINK_MESSAGE_INFO_SCALED_PRESSURE, MAVLINK_MESSAGE_INFO_WAYPOINT, MAVLINK_MESSAGE_INFO_WAYPOINT_REQUEST, MAVLINK_MESSAGE_INFO_WAYPOINT_SET_CURRENT, MAVLINK_MESSAGE_INFO_WAYPOINT_CURRENT, MAVLINK_MESSAGE_INFO_WAYPOINT_REQUEST_LIST, MAVLINK_MESSAGE_INFO_WAYPOINT_COUNT, MAVLINK_MESSAGE_INFO_WAYPOINT_CLEAR_ALL, MAVLINK_MESSAGE_INFO_WAYPOINT_REACHED, MAVLINK_MESSAGE_INFO_WAYPOINT_ACK, MAVLINK_MESSAGE_INFO_GPS_SET_GLOBAL_ORIGIN, MAVLINK_MESSAGE_INFO_GPS_LOCAL_ORIGIN_SET, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_SETPOINT_SET, MAVLINK_MESSAGE_INFO_LOCAL_POSITION_SETPOINT, MAVLINK_MESSAGE_INFO_CONTROL_STATUS, MAVLINK_MESSAGE_INFO_SAFETY_SET_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SAFETY_ALLOWED_AREA, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_THRUST, MAVLINK_MESSAGE_INFO_SET_ROLL_PITCH_YAW_SPEED_THRUST, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_THRUST_SETPOINT, MAVLINK_MESSAGE_INFO_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, {NULL}, {NULL}, {NULL}, MAVLINK_MESSAGE_INFO_NAV_CONTROLLER_OUTPUT, MAVLINK_MESSAGE_INFO_POSITION_TARGET, MAVLINK_MESSAGE_INFO_STATE_CORRECTION, MAVLINK_MESSAGE_INFO_SET_ALTITUDE, MAVLINK_MESSAGE_INFO_REQUEST_DATA_STREAM, MAVLINK_MESSAGE_INFO_HIL_STATE, MAVLINK_MESSAGE_INFO_HIL_CONTROLS, MAVLINK_MESSAGE_INFO_MANUAL_CONTROL, MAVLINK_MESSAGE_INFO_RC_CHANNELS_OVERRIDE, {NULL}, {NULL}, MAVLINK_MESSAGE_INFO_GLOBAL_POSITION_INT, MAVLINK_MESSAGE_INFO_VFR_HUD, MAVLINK_MESSAGE_INFO_COMMAND, MAVLINK_MESSAGE_INFO_COMMAND_ACK, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, MAVLINK_MESSAGE_INFO_OPTICAL_FLOW, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, MAVLINK_MESSAGE_INFO_OBJECT_DETECTION_EVENT, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, MAVLINK_MESSAGE_INFO_SENSOR_OFFSETS, MAVLINK_MESSAGE_INFO_SET_MAG_OFFSETS, MAVLINK_MESSAGE_INFO_MEMINFO, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, {NULL}, MAVLINK_MESSAGE_INFO_DEBUG_VECT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_FLOAT, MAVLINK_MESSAGE_INFO_NAMED_VALUE_INT, MAVLINK_MESSAGE_INFO_STATUSTEXT, MAVLINK_MESSAGE_INFO_DEBUG}
#endif
#include "../protocol.h"
@ -48,7 +48,6 @@ extern "C" {
#include "./mavlink_msg_sensor_offsets.h"
#include "./mavlink_msg_set_mag_offsets.h"
#include "./mavlink_msg_meminfo.h"
#include "./mavlink_msg_ap_adc.h"
#ifdef __cplusplus
}

View File

@ -1,254 +0,0 @@
// MESSAGE AP_ADC PACKING
#define MAVLINK_MSG_ID_AP_ADC 153
typedef struct __mavlink_ap_adc_t
{
uint16_t adc1; ///< ADC output 1
uint16_t adc2; ///< ADC output 2
uint16_t adc3; ///< ADC output 3
uint16_t adc4; ///< ADC output 4
uint16_t adc5; ///< ADC output 5
uint16_t adc6; ///< ADC output 6
} mavlink_ap_adc_t;
#define MAVLINK_MSG_ID_AP_ADC_LEN 12
#define MAVLINK_MSG_ID_153_LEN 12
#define MAVLINK_MESSAGE_INFO_AP_ADC { \
"AP_ADC", \
6, \
{ { "adc1", NULL, MAVLINK_TYPE_UINT16_T, 0, 0, offsetof(mavlink_ap_adc_t, adc1) }, \
{ "adc2", NULL, MAVLINK_TYPE_UINT16_T, 0, 2, offsetof(mavlink_ap_adc_t, adc2) }, \
{ "adc3", NULL, MAVLINK_TYPE_UINT16_T, 0, 4, offsetof(mavlink_ap_adc_t, adc3) }, \
{ "adc4", NULL, MAVLINK_TYPE_UINT16_T, 0, 6, offsetof(mavlink_ap_adc_t, adc4) }, \
{ "adc5", NULL, MAVLINK_TYPE_UINT16_T, 0, 8, offsetof(mavlink_ap_adc_t, adc5) }, \
{ "adc6", NULL, MAVLINK_TYPE_UINT16_T, 0, 10, offsetof(mavlink_ap_adc_t, adc6) }, \
} \
}
/**
* @brief Pack a ap_adc message
* @param system_id ID of this system
* @param component_id ID of this component (e.g. 200 for IMU)
* @param msg The MAVLink message to compress the data into
*
* @param adc1 ADC output 1
* @param adc2 ADC output 2
* @param adc3 ADC output 3
* @param adc4 ADC output 4
* @param adc5 ADC output 5
* @param adc6 ADC output 6
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_ap_adc_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
uint16_t adc1, uint16_t adc2, uint16_t adc3, uint16_t adc4, uint16_t adc5, uint16_t adc6)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[12];
_mav_put_uint16_t(buf, 0, adc1);
_mav_put_uint16_t(buf, 2, adc2);
_mav_put_uint16_t(buf, 4, adc3);
_mav_put_uint16_t(buf, 6, adc4);
_mav_put_uint16_t(buf, 8, adc5);
_mav_put_uint16_t(buf, 10, adc6);
memcpy(_MAV_PAYLOAD(msg), buf, 12);
#else
mavlink_ap_adc_t packet;
packet.adc1 = adc1;
packet.adc2 = adc2;
packet.adc3 = adc3;
packet.adc4 = adc4;
packet.adc5 = adc5;
packet.adc6 = adc6;
memcpy(_MAV_PAYLOAD(msg), &packet, 12);
#endif
msg->msgid = MAVLINK_MSG_ID_AP_ADC;
return mavlink_finalize_message(msg, system_id, component_id, 12);
}
/**
* @brief Pack a ap_adc message on a channel
* @param system_id ID of this system
* @param component_id ID of this component (e.g. 200 for IMU)
* @param chan The MAVLink channel this message was sent over
* @param msg The MAVLink message to compress the data into
* @param adc1 ADC output 1
* @param adc2 ADC output 2
* @param adc3 ADC output 3
* @param adc4 ADC output 4
* @param adc5 ADC output 5
* @param adc6 ADC output 6
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_ap_adc_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
mavlink_message_t* msg,
uint16_t adc1,uint16_t adc2,uint16_t adc3,uint16_t adc4,uint16_t adc5,uint16_t adc6)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[12];
_mav_put_uint16_t(buf, 0, adc1);
_mav_put_uint16_t(buf, 2, adc2);
_mav_put_uint16_t(buf, 4, adc3);
_mav_put_uint16_t(buf, 6, adc4);
_mav_put_uint16_t(buf, 8, adc5);
_mav_put_uint16_t(buf, 10, adc6);
memcpy(_MAV_PAYLOAD(msg), buf, 12);
#else
mavlink_ap_adc_t packet;
packet.adc1 = adc1;
packet.adc2 = adc2;
packet.adc3 = adc3;
packet.adc4 = adc4;
packet.adc5 = adc5;
packet.adc6 = adc6;
memcpy(_MAV_PAYLOAD(msg), &packet, 12);
#endif
msg->msgid = MAVLINK_MSG_ID_AP_ADC;
return mavlink_finalize_message_chan(msg, system_id, component_id, chan, 12);
}
/**
* @brief Encode a ap_adc struct into a message
*
* @param system_id ID of this system
* @param component_id ID of this component (e.g. 200 for IMU)
* @param msg The MAVLink message to compress the data into
* @param ap_adc C-struct to read the message contents from
*/
static inline uint16_t mavlink_msg_ap_adc_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_ap_adc_t* ap_adc)
{
return mavlink_msg_ap_adc_pack(system_id, component_id, msg, ap_adc->adc1, ap_adc->adc2, ap_adc->adc3, ap_adc->adc4, ap_adc->adc5, ap_adc->adc6);
}
/**
* @brief Send a ap_adc message
* @param chan MAVLink channel to send the message
*
* @param adc1 ADC output 1
* @param adc2 ADC output 2
* @param adc3 ADC output 3
* @param adc4 ADC output 4
* @param adc5 ADC output 5
* @param adc6 ADC output 6
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
static inline void mavlink_msg_ap_adc_send(mavlink_channel_t chan, uint16_t adc1, uint16_t adc2, uint16_t adc3, uint16_t adc4, uint16_t adc5, uint16_t adc6)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[12];
_mav_put_uint16_t(buf, 0, adc1);
_mav_put_uint16_t(buf, 2, adc2);
_mav_put_uint16_t(buf, 4, adc3);
_mav_put_uint16_t(buf, 6, adc4);
_mav_put_uint16_t(buf, 8, adc5);
_mav_put_uint16_t(buf, 10, adc6);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AP_ADC, buf, 12);
#else
mavlink_ap_adc_t packet;
packet.adc1 = adc1;
packet.adc2 = adc2;
packet.adc3 = adc3;
packet.adc4 = adc4;
packet.adc5 = adc5;
packet.adc6 = adc6;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_AP_ADC, (const char *)&packet, 12);
#endif
}
#endif
// MESSAGE AP_ADC UNPACKING
/**
* @brief Get field adc1 from ap_adc message
*
* @return ADC output 1
*/
static inline uint16_t mavlink_msg_ap_adc_get_adc1(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 0);
}
/**
* @brief Get field adc2 from ap_adc message
*
* @return ADC output 2
*/
static inline uint16_t mavlink_msg_ap_adc_get_adc2(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 2);
}
/**
* @brief Get field adc3 from ap_adc message
*
* @return ADC output 3
*/
static inline uint16_t mavlink_msg_ap_adc_get_adc3(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 4);
}
/**
* @brief Get field adc4 from ap_adc message
*
* @return ADC output 4
*/
static inline uint16_t mavlink_msg_ap_adc_get_adc4(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 6);
}
/**
* @brief Get field adc5 from ap_adc message
*
* @return ADC output 5
*/
static inline uint16_t mavlink_msg_ap_adc_get_adc5(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 8);
}
/**
* @brief Get field adc6 from ap_adc message
*
* @return ADC output 6
*/
static inline uint16_t mavlink_msg_ap_adc_get_adc6(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 10);
}
/**
* @brief Decode a ap_adc message into a struct
*
* @param msg The message to decode
* @param ap_adc C-struct to decode the message contents into
*/
static inline void mavlink_msg_ap_adc_decode(const mavlink_message_t* msg, mavlink_ap_adc_t* ap_adc)
{
#if MAVLINK_NEED_BYTE_SWAP
ap_adc->adc1 = mavlink_msg_ap_adc_get_adc1(msg);
ap_adc->adc2 = mavlink_msg_ap_adc_get_adc2(msg);
ap_adc->adc3 = mavlink_msg_ap_adc_get_adc3(msg);
ap_adc->adc4 = mavlink_msg_ap_adc_get_adc4(msg);
ap_adc->adc5 = mavlink_msg_ap_adc_get_adc5(msg);
ap_adc->adc6 = mavlink_msg_ap_adc_get_adc6(msg);
#else
memcpy(ap_adc, _MAV_PAYLOAD(msg), 12);
#endif
}

View File

@ -185,65 +185,11 @@ static void mavlink_test_meminfo(uint8_t system_id, uint8_t component_id, mavlin
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
}
static void mavlink_test_ap_adc(uint8_t system_id, uint8_t component_id, mavlink_message_t *last_msg)
{
mavlink_message_t msg;
uint8_t buffer[MAVLINK_MAX_PACKET_LEN];
uint16_t i;
mavlink_ap_adc_t packet_in = {
17235,
17339,
17443,
17547,
17651,
17755,
};
mavlink_ap_adc_t packet1, packet2;
memset(&packet1, 0, sizeof(packet1));
packet1.adc1 = packet_in.adc1;
packet1.adc2 = packet_in.adc2;
packet1.adc3 = packet_in.adc3;
packet1.adc4 = packet_in.adc4;
packet1.adc5 = packet_in.adc5;
packet1.adc6 = packet_in.adc6;
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_ap_adc_encode(system_id, component_id, &msg, &packet1);
mavlink_msg_ap_adc_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_ap_adc_pack(system_id, component_id, &msg , packet1.adc1 , packet1.adc2 , packet1.adc3 , packet1.adc4 , packet1.adc5 , packet1.adc6 );
mavlink_msg_ap_adc_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_ap_adc_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.adc1 , packet1.adc2 , packet1.adc3 , packet1.adc4 , packet1.adc5 , packet1.adc6 );
mavlink_msg_ap_adc_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_to_send_buffer(buffer, &msg);
for (i=0; i<mavlink_msg_get_send_buffer_length(&msg); i++) {
comm_send_ch(MAVLINK_COMM_0, buffer[i]);
}
mavlink_msg_ap_adc_decode(last_msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_ap_adc_send(MAVLINK_COMM_1 , packet1.adc1 , packet1.adc2 , packet1.adc3 , packet1.adc4 , packet1.adc5 , packet1.adc6 );
mavlink_msg_ap_adc_decode(last_msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
}
static void mavlink_test_ardupilotmega(uint8_t system_id, uint8_t component_id, mavlink_message_t *last_msg)
{
mavlink_test_sensor_offsets(system_id, component_id, last_msg);
mavlink_test_set_mag_offsets(system_id, component_id, last_msg);
mavlink_test_meminfo(system_id, component_id, last_msg);
mavlink_test_ap_adc(system_id, component_id, last_msg);
}
#ifdef __cplusplus

View File

@ -5,7 +5,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Sat Sep 10 18:09:49 2011"
#define MAVLINK_BUILD_DATE "Sun Sep 4 18:16:41 2011"
#define MAVLINK_WIRE_PROTOCOL_VERSION "0.9"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 101

View File

@ -5,7 +5,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Sat Sep 10 18:09:49 2011"
#define MAVLINK_BUILD_DATE "Sun Sep 4 18:16:41 2011"
#define MAVLINK_WIRE_PROTOCOL_VERSION "0.9"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 101

View File

@ -41,15 +41,5 @@
<field type="uint16_t" name="freemem">free memory</field>
</message>
<message id="153" name="AP_ADC">
<description>raw ADC output</description>
<field type="uint16_t" name="adc1">ADC output 1</field>
<field type="uint16_t" name="adc2">ADC output 2</field>
<field type="uint16_t" name="adc3">ADC output 3</field>
<field type="uint16_t" name="adc4">ADC output 4</field>
<field type="uint16_t" name="adc5">ADC output 5</field>
<field type="uint16_t" name="adc6">ADC output 6</field>
</message>
</messages>
</mavlink>

View File

@ -1,31 +0,0 @@
<?xml version='1.0'?>
<mavlink>
<version>3</version>
<messages>
<message id="0" name="TEST_TYPES">
<description>Test all field types</description>
<field type="char" name="c">char</field>
<field type="char[10]" name="s">string</field>
<field type="uint8_t" name="u8">uint8_t</field>
<field type="uint16_t" name="u16">uint16_t</field>
<field type="uint32_t" name="u32" print_format="0x%08x">uint32_t</field>
<field type="uint64_t" name="u64">uint64_t</field>
<field type="int8_t" name="s8">int8_t</field>
<field type="int16_t" name="s16">int16_t</field>
<field type="int32_t" name="s32">int32_t</field>
<field type="int64_t" name="s64">int64_t</field>
<field type="float" name="f">float</field>
<field type="double" name="d">double</field>
<field type="uint8_t[3]" name="u8_array">uint8_t_array</field>
<field type="uint16_t[3]" name="u16_array">uint16_t_array</field>
<field type="uint32_t[3]" name="u32_array">uint32_t_array</field>
<field type="uint64_t[3]" name="u64_array">uint64_t_array</field>
<field type="int8_t[3]" name="s8_array">int8_t_array</field>
<field type="int16_t[3]" name="s16_array">int16_t_array</field>
<field type="int32_t[3]" name="s32_array">int32_t_array</field>
<field type="int64_t[3]" name="s64_array">int64_t_array</field>
<field type="float[3]" name="f_array">float_array</field>
<field type="double[3]" name="d_array">double_array</field>
</message>
</messages>
</mavlink>