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ardupilot/APMrover2/Parameters.pde

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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: t -*-
/*
ArduPlane parameter definitions
This firmware is free software; you can redistribute it and/or
modify it under the terms of the GNU Lesser General Public
License as published by the Free Software Foundation; either
version 2.1 of the License, or (at your option) any later version.
*/
#define GSCALAR(v, name, def) { g.v.vtype, name, Parameters::k_param_ ## v, &g.v, {def_value:def} }
#define GGROUP(v, name, class) { AP_PARAM_GROUP, name, Parameters::k_param_ ## v, &g.v, {group_info:class::var_info} }
#define GOBJECT(v, name, class) { AP_PARAM_GROUP, name, Parameters::k_param_ ## v, &v, {group_info:class::var_info} }
const AP_Param::Info var_info[] PROGMEM = {
GSCALAR(format_version, "FORMAT_VERSION", 0),
GSCALAR(software_type, "SYSID_SW_TYPE", Parameters::k_software_type),
GSCALAR(sysid_this_mav, "SYSID_THISMAV", MAV_SYSTEM_ID),
GSCALAR(sysid_my_gcs, "SYSID_MYGCS", 255),
// @Param: SERIAL3_BAUD
// @DisplayName: Telemetry Baud Rate
// @Description: The baud rate used on the telemetry port
// @Values: 1:1200,2:2400,4:4800,9:9600,19:19200,38:38400,57:57600,111:111100,115:115200
// @User: Standard
GSCALAR(serial3_baud, "SERIAL3_BAUD", SERIAL3_BAUD/1000),
// @Param: TELEM_DELAY
// @DisplayName: Telemetry startup delay
// @Description: The amount of time (in seconds) to delay radio telemetry to prevent an Xbee bricking on power up
// @User: Standard
// @Units: seconds
// @Range: 0 10
// @Increment: 1
GSCALAR(telem_delay, "TELEM_DELAY", 0),
// @Param: MANUAL_LEVEL
// @DisplayName: Manual Level
// @Description: Setting this to Disabled(0) will enable autolevel on every boot. Setting it to Enabled(1) will do a calibration only when you tell it to
// @Values: 0:Disabled,1:Enabled
// @User: Advanced
GSCALAR(manual_level, "MANUAL_LEVEL", 0),
// @Param: XTRK_GAIN_SC
// @DisplayName: Crosstrack Gain
// @Description: The scale between distance off the line and angle to meet the line (in Degrees * 100)
// @Range: 0 2000
// @Increment: 1
// @User: Standard
GSCALAR(crosstrack_gain, "XTRK_GAIN_SC", XTRACK_GAIN_SCALED),
// @Param: XTRK_ANGLE_CD
// @DisplayName: Crosstrack Entry Angle
// @Description: Maximum angle used to correct for track following.
// @Units: centi-Degrees
// @Range: 0 9000
// @Increment: 1
// @User: Standard
GSCALAR(crosstrack_entry_angle, "XTRK_ANGLE_CD", XTRACK_ENTRY_ANGLE_CENTIDEGREE),
GSCALAR(command_total, "CMD_TOTAL", 0),
GSCALAR(command_index, "CMD_INDEX", 0),
GSCALAR(waypoint_radius, "WP_RADIUS", WP_RADIUS_DEFAULT),
// @Param: THR_MIN
// @DisplayName: Minimum Throttle
// @Description: The minimum throttle setting to which the autopilot will apply.
// @Units: Percent
// @Range: 0 100
// @Increment: 1
// @User: Standard
GSCALAR(throttle_min, "THR_MIN", THROTTLE_MIN),
// @Param: THR_MAX
// @DisplayName: Maximum Throttle
// @Description: The maximum throttle setting to which the autopilot will apply.
// @Units: Percent
// @Range: 0 100
// @Increment: 1
// @User: Standard
GSCALAR(throttle_max, "THR_MAX", THROTTLE_MAX),
// @Param: THR_SLEWRATE
// @DisplayName: Throttle slew rate
// @Description: maximum percentage change in throttle per second. A setting of 10 means to not change the throttle by more than 10% of the full throttle range in one second
// @Units: Percent
// @Range: 0 100
// @Increment: 1
// @User: Standard
GSCALAR(throttle_slewrate, "THR_SLEWRATE", THROTTLE_SLEW_LIMIT),
// @Param: THR_FAILSAFE
// @DisplayName: Throttle Failsafe Enable
// @Description: The throttle failsafe allows you to configure a software failsafe activated by a setting on the throttle input channel
// @Values: 0:Disabled,1:Enabled
// @User: Standard
GSCALAR(throttle_fs_enabled, "THR_FAILSAFE", THROTTLE_FAILSAFE),
// @Param: THR_FS_VALUE
// @DisplayName: Throttle Failsafe Value
// @Description: The PWM level on channel 3 below which throttle sailsafe triggers
// @User: Standard
GSCALAR(throttle_fs_value, "THR_FS_VALUE", THROTTLE_FS_VALUE),
// @Param: TRIM_THROTTLE
// @DisplayName: Throttle cruise percentage
// @Description: The target percentage of throttle to apply for normal flight
// @Units: Percent
// @Range: 0 100
// @Increment: 1
// @User: Standard
GSCALAR(throttle_cruise, "TRIM_THROTTLE", THROTTLE_CRUISE),
// @Param: FS_SHORT_ACTN
// @DisplayName: Short failsafe action
// @Description: The action to take on a short (1 second) failsafe event
// @Values: 0:None,1:ReturnToLaunch
// @User: Standard
GSCALAR(short_fs_action, "FS_SHORT_ACTN", SHORT_FAILSAFE_ACTION),
// @Param: FS_LONG_ACTN
// @DisplayName: Long failsafe action
// @Description: The action to take on a long (20 second) failsafe event
// @Values: 0:None,1:ReturnToLaunch
// @User: Standard
GSCALAR(long_fs_action, "FS_LONG_ACTN", LONG_FAILSAFE_ACTION),
// @Param: FS_GCS_ENABL
// @DisplayName: GCS failsafe enable
// @Description: Enable ground control station telemetry failsafe. Failsafe will trigger after 20 seconds of no MAVLink heartbeat messages
// @Values: 0:Disabled,1:Enabled
// @User: Standard
GSCALAR(gcs_heartbeat_fs_enabled, "FS_GCS_ENABL", GCS_HEARTBEAT_FAILSAFE),
// @Param: FLTMODE_CH
// @DisplayName: Flightmode channel
// @Description: RC Channel to use for flight mode control
// @User: Advanced
GSCALAR(flight_mode_channel, "FLTMODE_CH", FLIGHT_MODE_CHANNEL),
// @Param: FLTMODE1
// @DisplayName: FlightMode1
// @Values: 0:Manual,1:CIRCLE,2:STABILIZE,5:FBWA,6:FBWB,10:Auto,11:RTL,12:Loiter,15:Guided
// @User: Standard
// @Description: Flight mode for switch position 1 (910 to 1230 and above 2049)
GSCALAR(flight_mode1, "FLTMODE1", FLIGHT_MODE_1),
// @Param: FLTMODE2
// @DisplayName: FlightMode2
// @Description: Flight mode for switch position 2 (1231 to 1360)
// @Values: 0:Manual,1:CIRCLE,2:STABILIZE,5:FBWA,6:FBWB,10:Auto,11:RTL,12:Loiter,15:Guided
// @User: Standard
GSCALAR(flight_mode2, "FLTMODE2", FLIGHT_MODE_2),
// @Param: FLTMODE3
// @DisplayName: FlightMode3
// @Description: Flight mode for switch position 3 (1361 to 1490)
// @Values: 0:Manual,1:CIRCLE,2:STABILIZE,5:FBWA,6:FBWB,10:Auto,11:RTL,12:Loiter,15:Guided
// @User: Standard
GSCALAR(flight_mode3, "FLTMODE3", FLIGHT_MODE_3),
// @Param: FLTMODE4
// @DisplayName: FlightMode4
// @Description: Flight mode for switch position 4 (1491 to 1620)
// @Values: 0:Manual,1:CIRCLE,2:STABILIZE,5:FBWA,6:FBWB,10:Auto,11:RTL,12:Loiter,15:Guided
// @User: Standard
GSCALAR(flight_mode4, "FLTMODE4", FLIGHT_MODE_4),
// @Param: FLTMODE5
// @DisplayName: FlightMode5
// @Description: Flight mode for switch position 5 (1621 to 1749)
// @Values: 0:Manual,1:CIRCLE,2:STABILIZE,5:FBWA,6:FBWB,10:Auto,11:RTL,12:Loiter,15:Guided
// @User: Standard
GSCALAR(flight_mode5, "FLTMODE5", FLIGHT_MODE_5),
// @Param: FLTMODE6
// @DisplayName: FlightMode6
// @Description: Flight mode for switch position 6 (1750 to 2049)
// @Values: 0:Manual,1:CIRCLE,2:STABILIZE,5:FBWA,6:FBWB,10:Auto,11:RTL,12:Loiter,15:Guided
// @User: Standard
GSCALAR(flight_mode6, "FLTMODE6", FLIGHT_MODE_6),
GSCALAR(roll_limit, "LIM_ROLL_CD", HEAD_MAX_CENTIDEGREE),
GSCALAR(pitch_limit_max, "LIM_PITCH_MAX", PITCH_MAX_CENTIDEGREE),
GSCALAR(pitch_limit_min, "LIM_PITCH_MIN", PITCH_MIN_CENTIDEGREE),
GSCALAR(auto_trim, "TRIM_AUTO", AUTO_TRIM),
GSCALAR(num_resets, "SYS_NUM_RESETS", 0),
GSCALAR(log_bitmask, "LOG_BITMASK", DEFAULT_LOG_BITMASK),
GSCALAR(log_last_filenumber, "LOG_LASTFILE", 0),
GSCALAR(reset_switch_chan, "RST_SWITCH_CH", 0),
GSCALAR(airspeed_cruise, "TRIM_ARSPD_CM", AIRSPEED_CRUISE_CM),
GSCALAR(min_gndspeed, "MIN_GNDSPD_CM", MIN_GNDSPEED_CM),
GSCALAR(ch7_option, "CH7_OPT", CH7_OPTION),
GSCALAR(compass_enabled, "MAG_ENABLE", MAGNETOMETER),
GSCALAR(battery_monitoring, "BATT_MONITOR", DISABLED),
GSCALAR(volt_div_ratio, "VOLT_DIVIDER", VOLT_DIV_RATIO),
GSCALAR(curr_amp_per_volt, "AMP_PER_VOLT", CURR_AMP_PER_VOLT),
GSCALAR(input_voltage, "INPUT_VOLTS", INPUT_VOLTAGE),
GSCALAR(pack_capacity, "BATT_CAPACITY", HIGH_DISCHARGE),
// @Param: BATT_VOLT_PIN
// @DisplayName: Battery Voltage sensing pin
// @Description: Setting this to 0 ~ 13 will enable battery current sensing on pins A0 ~ A13.
// @Values: -1:Disabled, 0:A0, 1:A1, 13:A13
// @User: Standard
GSCALAR(battery_volt_pin, "BATT_VOLT_PIN", 1),
// @Param: BATT_CURR_PIN
// @DisplayName: Battery Current sensing pin
// @Description: Setting this to 0 ~ 13 will enable battery current sensing on pins A0 ~ A13.
// @Values: -1:Disabled, 1:A1, 2:A2, 12:A12
// @User: Standard
GSCALAR(battery_curr_pin, "BATT_CURR_PIN", 2),
// @Param: RSSI_PIN
// @DisplayName: Receiver RSSI sensing pin
// @Description: This selects an analog pin for the receiver RSSI voltage. It assumes the voltage is 5V for max rssi, 0V for minimum
// @Values: -1:Disabled, 0:A0, 1:A1, 13:A13
// @User: Standard
GSCALAR(rssi_pin, "RSSI_PIN", -1),
#if HIL_MODE != HIL_MODE_ATTITUDE
#if CONFIG_SONAR == ENABLED
// @Param: SONAR_ENABLE
// @DisplayName: Enable Sonar
// @Description: Setting this to Enabled(1) will enable the sonar. Setting this to Disabled(0) will disable the sonar
// @Values: 0:Disabled,1:Enabled
// @User: Standard
GSCALAR(sonar_enabled, "SONAR_ENABLE", SONAR_ENABLED),
GSCALAR(sonar_type, "SONAR_TYPE", AP_RANGEFINDER_MAXSONARXL),
#endif
#endif
// ************************************************************
// APMrover parameters - JLN update
GSCALAR(auto_wp_radius, "ROV_AWPR_NAV", AUTO_WP_RADIUS),
GSCALAR(sonar_trigger, "ROV_SONAR_TRIG", SONAR_TRIGGER),
GSCALAR(turn_gain, "ROV_GAIN", TURN_GAIN),
GSCALAR(booster, "ROV_BOOSTER", BOOSTER),
// ************************************************************
GGROUP(channel_roll, "RC1_", RC_Channel),
GGROUP(channel_pitch, "RC2_", RC_Channel),
GGROUP(channel_throttle, "RC3_", RC_Channel),
GGROUP(channel_rudder, "RC4_", RC_Channel),
GGROUP(rc_5, "RC5_", RC_Channel_aux),
GGROUP(rc_6, "RC6_", RC_Channel_aux),
GGROUP(rc_7, "RC7_", RC_Channel_aux),
GGROUP(rc_8, "RC8_", RC_Channel_aux),
GGROUP(pidNavRoll, "HDNG2RLL_", PID),
GGROUP(pidServoRoll, "RLL2SRV_", PID),
GGROUP(pidServoPitch, "PTCH2SRV_", PID),
GGROUP(pidNavPitchAirspeed, "ARSP2PTCH_", PID),
GGROUP(pidServoRudder, "YW2SRV_", PID),
GGROUP(pidTeThrottle, "ENRGY2THR_", PID),
GGROUP(pidNavPitchAltitude, "ALT2PTCH_", PID),
// variables not in the g class which contain EEPROM saved variables
GOBJECT(compass, "COMPASS_", Compass),
GOBJECT(gcs0, "SR0_", GCS_MAVLINK),
GOBJECT(gcs3, "SR3_", GCS_MAVLINK),
#if HIL_MODE == HIL_MODE_DISABLED
// @Group: INS_
// @Path: ../libraries/AP_InertialSensor/AP_InertialSensor.cpp
GOBJECT(ins, "INS_", AP_InertialSensor),
#endif
#if CONFIG_HAL_BOARD == HAL_BOARD_AVR_SITL
// @Group: SIM_
// @Path: ../libraries/SITL/SITL.cpp
GOBJECT(sitl, "SIM_", SITL),
#endif
// @Group: AHRS_
// @Path: ../libraries/AP_AHRS/AP_AHRS.cpp
GOBJECT(ahrs, "AHRS_", AP_AHRS),
AP_VAREND
};
static void load_parameters(void)
{
if (!g.format_version.load() ||
g.format_version != Parameters::k_format_version) {
// erase all parameters
cliSerial->printf_P(PSTR("Firmware change: erasing EEPROM...\n"));
AP_Param::erase_all();
// save the current format version
g.format_version.set_and_save(Parameters::k_format_version);
cliSerial->println_P(PSTR("done."));
} else {
unsigned long before = micros();
// Load all auto-loaded EEPROM variables
AP_Param::load_all();
cliSerial->printf_P(PSTR("load_all took %luus\n"), micros() - before);
}
}
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