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Parameters.pde
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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
/*
This program is free software: you can redistribute it and/or modify
it under the terms of the GNU General Public License as published by
the Free Software Foundation, either version 3 of the License, or
(at your option) any later version.
This program is distributed in the hope that it will be useful,
but WITHOUT ANY WARRANTY; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
GNU General Public License for more details.
You should have received a copy of the GNU General Public License
along with this program. If not, see <http://www.gnu.org/licenses/>.
*/
/*
* ArduCopter parameter definitions
*
*/
#define GSCALAR(v, name, def) { g.v.vtype, name, Parameters::k_param_ ## v, &g.v, {def_value : def} }
#define ASCALAR(v, name, def) { aparm.v.vtype, name, Parameters::k_param_ ## v, &aparm.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} }
#define GOBJECTN(v, pname, name, class) { AP_PARAM_GROUP, name, Parameters::k_param_ ## pname, &v, {group_info : class::var_info} }
const AP_Param::Info var_info[] PROGMEM = {
// @Param: SYSID_SW_MREV
// @DisplayName: Eeprom format version number
// @Description: This value is incremented when changes are made to the eeprom format
// @User: Advanced
GSCALAR(format_version, "SYSID_SW_MREV", 0),
// @Param: SYSID_SW_TYPE
// @DisplayName: Software Type
// @Description: This is used by the ground station to recognise the software type (eg ArduPlane vs ArduCopter)
// @User: Advanced
GSCALAR(software_type, "SYSID_SW_TYPE", Parameters::k_software_type),
// @Param: SYSID_THISMAV
// @DisplayName: Mavlink version
// @Description: Allows reconising the mavlink version
// @Range: 1 255
// @User: Advanced
GSCALAR(sysid_this_mav, "SYSID_THISMAV", MAV_SYSTEM_ID),
// @Param: SYSID_MYGCS
// @DisplayName: My ground station number
// @Description: Allows restricting radio overrides to only come from my ground station
// @Range: 1 255
// @User: Advanced
GSCALAR(sysid_my_gcs, "SYSID_MYGCS", 255),
// @Param: SERIAL1_BAUD
// @DisplayName: Telemetry Baud Rate
// @Description: The baud rate used on the first telemetry port
// @Values: 1:1200,2:2400,4:4800,9:9600,19:19200,38:38400,57:57600,111:111100,115:115200
// @User: Standard
GSCALAR(serial1_baud, "SERIAL1_BAUD", SERIAL1_BAUD/1000),
#if MAVLINK_COMM_NUM_BUFFERS > 2
// @Param: SERIAL2_BAUD
// @DisplayName: Telemetry Baud Rate
// @Description: The baud rate used on the seconds telemetry port
// @Values: 1:1200,2:2400,4:4800,9:9600,19:19200,38:38400,57:57600,111:111100,115:115200
// @User: Standard
GSCALAR(serial2_baud, "SERIAL2_BAUD", SERIAL2_BAUD/1000),
#endif
// @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: Advanced
// @Units: seconds
// @Range: 0 10
// @Increment: 1
GSCALAR(telem_delay, "TELEM_DELAY", 0),
// @Param: RTL_ALT
// @DisplayName: RTL Altitude
// @Description: The minimum altitude the model will move to before Returning to Launch. Set to zero to return at current altitude.
// @Units: Centimeters
// @Range: 0 8000
// @Increment: 1
// @User: Standard
GSCALAR(rtl_altitude, "RTL_ALT", RTL_ALT),
// @Param: SONAR_ENABLE
// @DisplayName: Sonar enable/disable
// @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", DISABLED),
// @Param: SONAR_TYPE
// @DisplayName: Sonar type
// @Description: Used to adjust scaling to match the sonar used (only Maxbotix sonars are supported at this time)
// @Values: 0:XL-EZ0 / XL-EZ4,1:LV-EZ0,2:XLL-EZ0,3:HRLV
// @User: Standard
GSCALAR(sonar_type, "SONAR_TYPE", AP_RANGEFINDER_MAXSONARXL),
// @Param: SONAR_GAIN
// @DisplayName: Sonar gain
// @Description: Used to adjust the speed with which the target altitude is changed when objects are sensed below the copter
// @Range: 0.01 2.0
// @Increment: 0.01
// @User: Standard
GSCALAR(sonar_gain, "SONAR_GAIN", SONAR_GAIN_DEFAULT),
// @Param: FS_BATT_ENABLE
// @DisplayName: Battery Failsafe Enable
// @Description: Controls whether failsafe will be invoked when battery voltage or current runs low
// @Values: 0:Disabled,1:Land,2:RTL
// @User: Standard
GSCALAR(failsafe_battery_enabled, "FS_BATT_ENABLE", FS_BATT_DISABLED),
// @Param: FS_BATT_VOLTAGE
// @DisplayName: Failsafe battery voltage
// @Description: Battery voltage to trigger failsafe. Set to 0 to disable battery voltage failsafe. If the battery voltage drops below this voltage then the copter will RTL
// @Units: Volts
// @Increment: 0.1
// @User: Standard
GSCALAR(fs_batt_voltage, "FS_BATT_VOLTAGE", FS_BATT_VOLTAGE_DEFAULT),
// @Param: FS_BATT_MAH
// @DisplayName: Failsafe battery milliAmpHours
// @Description: Battery capacity remaining to trigger failsafe. Set to 0 to disable battery remaining failsafe. If the battery remaining drops below this level then the copter will RTL
// @Units: mAh
// @Increment: 50
// @User: Standard
GSCALAR(fs_batt_mah, "FS_BATT_MAH", FS_BATT_MAH_DEFAULT),
// @Param: FS_GPS_ENABLE
// @DisplayName: GPS Failsafe Enable
// @Description: Controls what action will be taken if GPS signal is lost for at least 5 seconds
// @Values: 0:Disabled,1:Land,2:AltHold,3:Land even from Stabilize
// @User: Standard
GSCALAR(failsafe_gps_enabled, "FS_GPS_ENABLE", FS_GPS_LAND),
// @Param: FS_GCS_ENABLE
// @DisplayName: Ground Station Failsafe Enable
// @Description: Controls whether failsafe will be invoked (and what action to take) when connection with Ground station is lost for at least 5 seconds
// @Values: 0:Disabled,1:Enabled always RTL,2:Enabled Continue with Mission in Auto Mode
// @User: Standard
GSCALAR(failsafe_gcs, "FS_GCS_ENABLE", FS_GCS_DISABLED),
// @Param: GPS_HDOP_GOOD
// @DisplayName: GPS Hdop Good
// @Description: GPS Hdop value at or below this value represent a good position. Used for pre-arm checks
// @Range: 100 900
// @User: Advanced
GSCALAR(gps_hdop_good, "GPS_HDOP_GOOD", GPS_HDOP_GOOD_DEFAULT),
// @Param: MAG_ENABLE
// @DisplayName: Compass enable/disable
// @Description: Setting this to Enabled(1) will enable the compass. Setting this to Disabled(0) will disable the compass
// @Values: 0:Disabled,1:Enabled
// @User: Standard
GSCALAR(compass_enabled, "MAG_ENABLE", MAGNETOMETER),
// @Param: FLOW_ENABLE
// @DisplayName: Optical Flow enable/disable
// @Description: Setting this to Enabled(1) will enable optical flow. Setting this to Disabled(0) will disable optical flow
// @Values: 0:Disabled,1:Enabled
// @User: Standard
GSCALAR(optflow_enabled, "FLOW_ENABLE", DISABLED),
// @Param: SUPER_SIMPLE
// @DisplayName: Super Simple Mode
// @Description: Bitmask to enable Super Simple mode for some flight modes. Setting this to Disabled(0) will disable Super Simple Mode
// @Values: 0:Disabled,1:Mode1,2:Mode2,3:Mode1+2,4:Mode3,5:Mode1+3,6:Mode2+3,7:Mode1+2+3,8:Mode4,9:Mode1+4,10:Mode2+4,11:Mode1+2+4,12:Mode3+4,13:Mode1+3+4,14:Mode2+3+4,15:Mode1+2+3+4,16:Mode5,17:Mode1+5,18:Mode2+5,19:Mode1+2+5,20:Mode3+5,21:Mode1+3+5,22:Mode2+3+5,23:Mode1+2+3+5,24:Mode4+5,25:Mode1+4+5,26:Mode2+4+5,27:Mode1+2+4+5,28:Mode3+4+5,29:Mode1+3+4+5,30:Mode2+3+4+5,31:Mode1+2+3+4+5,32:Mode6,33:Mode1+6,34:Mode2+6,35:Mode1+2+6,36:Mode3+6,37:Mode1+3+6,38:Mode2+3+6,39:Mode1+2+3+6,40:Mode4+6,41:Mode1+4+6,42:Mode2+4+6,43:Mode1+2+4+6,44:Mode3+4+6,45:Mode1+3+4+6,46:Mode2+3+4+6,47:Mode1+2+3+4+6,48:Mode5+6,49:Mode1+5+6,50:Mode2+5+6,51:Mode1+2+5+6,52:Mode3+5+6,53:Mode1+3+5+6,54:Mode2+3+5+6,55:Mode1+2+3+5+6,56:Mode4+5+6,57:Mode1+4+5+6,58:Mode2+4+5+6,59:Mode1+2+4+5+6,60:Mode3+4+5+6,61:Mode1+3+4+5+6,62:Mode2+3+4+5+6,63:Mode1+2+3+4+5+6
// @User: Standard
GSCALAR(super_simple, "SUPER_SIMPLE", 0),
// @Param: RTL_ALT_FINAL
// @DisplayName: RTL Final Altitude
// @Description: This is the altitude the vehicle will move to as the final stage of Returning to Launch or after completing a mission. Set to zero to land.
// @Units: Centimeters
// @Range: -1 1000
// @Increment: 1
// @User: Standard
GSCALAR(rtl_alt_final, "RTL_ALT_FINAL", RTL_ALT_FINAL),
// @Param: RSSI_PIN
// @DisplayName: Receiver RSSI sensing pin
// @Description: This selects an analog pin for the receiver RSSI voltage. It assumes the voltage is RSSI_RANGE for max rssi, 0V for minimum
// @Values: -1:Disabled, 0:A0, 1:A1, 2:A2, 13:A13
// @User: Standard
GSCALAR(rssi_pin, "RSSI_PIN", -1),
// @Param: RSSI_RANGE
// @DisplayName: Receiver RSSI voltage range
// @Description: Receiver RSSI voltage range
// @Units: Volt
// @Values: 3.3:3.3V, 5.0:5V
// @User: Standard
GSCALAR(rssi_range, "RSSI_RANGE", 5.0),
// @Param: WP_YAW_BEHAVIOR
// @DisplayName: Yaw behaviour during missions
// @Description: Determines how the autopilot controls the yaw during missions and RTL
// @Values: 0:Never change yaw, 1:Face next waypoint, 2:Face next waypoint except RTL, 3:Face along GPS course
// @User: Standard
GSCALAR(wp_yaw_behavior, "WP_YAW_BEHAVIOR", WP_YAW_BEHAVIOR_DEFAULT),
// @Param: WP_TOTAL
// @DisplayName: Waypoint Total
// @Description: Total number of commands in the mission stored in the eeprom. Do not update this parameter directly!
// @User: Advanced
GSCALAR(command_total, "WP_TOTAL", 0),
// @Param: WP_INDEX
// @DisplayName: Waypoint Index
// @Description: The index number of the command that is currently being executed. Do not update this parameter directly!
// @User: Advanced
GSCALAR(command_index, "WP_INDEX", 0),
// @Param: RTL_LOIT_TIME
// @DisplayName: RTL loiter time
// @Description: Time (in milliseconds) to loiter above home before begining final descent
// @Units: ms
// @Range: 0 60000
// @Increment: 1000
// @User: Standard
GSCALAR(rtl_loiter_time, "RTL_LOIT_TIME", RTL_LOITER_TIME),
// @Param: LAND_SPEED
// @DisplayName: Land speed
// @Description: The descent speed for the final stage of landing in cm/s
// @Units: cm/s
// @Range: 30 200
// @Increment: 10
// @User: Standard
GSCALAR(land_speed, "LAND_SPEED", LAND_SPEED),
// @Param: PILOT_VELZ_MAX
// @DisplayName: Pilot maximum vertical speed
// @Description: The maximum vertical velocity the pilot may request in cm/s
// @Units: Centimeters/Second
// @Range: 10 500
// @Increment: 10
// @User: Standard
GSCALAR(pilot_velocity_z_max, "PILOT_VELZ_MAX", PILOT_VELZ_MAX),
// @Param: THR_MIN
// @DisplayName: Throttle Minimum
// @Description: The minimum throttle that will be sent to the motors to keep them spinning
// @Units: Percent*10
// @Range: 0 300
// @Increment: 1
// @User: Standard
GSCALAR(throttle_min, "THR_MIN", THR_MIN_DEFAULT),
// @Param: THR_MAX
// @DisplayName: Throttle Maximum
// @Description: The maximum throttle that will be sent to the motors. This should normally be left as 1000.
// @Units: Percent*10
// @Range: 800 1000
// @Increment: 1
// @User: Advanced
GSCALAR(throttle_max, "THR_MAX", THR_MAX_DEFAULT),
// @Param: FS_THR_ENABLE
// @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 always RTL,2:Enabled Continue with Mission in Auto Mode,3:Enabled always LAND
// @User: Standard
GSCALAR(failsafe_throttle, "FS_THR_ENABLE", FS_THR_DISABLED),
// @Param: FS_THR_VALUE
// @DisplayName: Throttle Failsafe Value
// @Description: The PWM level on channel 3 below which throttle sailsafe triggers
// @Range: 925 1100
// @Units: pwm
// @Increment: 1
// @User: Standard
GSCALAR(failsafe_throttle_value, "FS_THR_VALUE", FS_THR_VALUE_DEFAULT),
// @Param: TRIM_THROTTLE
// @DisplayName: Throttle Trim
// @Description: The autopilot's estimate of the throttle required to maintain a level hover. Calculated automatically from the pilot's throttle input while in stabilize mode
// @Range: 0 1000
// @Units: Percent*10
// @User: Advanced
GSCALAR(throttle_cruise, "TRIM_THROTTLE", THROTTLE_CRUISE),
// @Param: THR_MID
// @DisplayName: Throttle Mid Position
// @Description: The throttle output (0 ~ 1000) when throttle stick is in mid position. Used to scale the manual throttle so that the mid throttle stick position is close to the throttle required to hover
// @User: Standard
// @Range: 300 700
// @Units: Percent*10
// @Increment: 1
GSCALAR(throttle_mid, "THR_MID", THR_MID_DEFAULT),
// @Param: FLTMODE1
// @DisplayName: Flight Mode 1
// @Description: Flight mode when Channel 5 pwm is <= 1230
// @Values: 0:Stabilize,1:Acro,2:AltHold,3:Auto,4:Guided,5:Loiter,6:RTL,7:Circle,9:Land,10:OF_Loiter,11:Drift,13:Sport
// @User: Standard
GSCALAR(flight_mode1, "FLTMODE1", FLIGHT_MODE_1),
// @Param: FLTMODE2
// @DisplayName: Flight Mode 2
// @Description: Flight mode when Channel 5 pwm is >1230, <= 1360
// @Values: 0:Stabilize,1:Acro,2:AltHold,3:Auto,4:Guided,5:Loiter,6:RTL,7:Circle,9:Land,10:OF_Loiter,11:Drift,13:Sport
// @User: Standard
GSCALAR(flight_mode2, "FLTMODE2", FLIGHT_MODE_2),
// @Param: FLTMODE3
// @DisplayName: Flight Mode 3
// @Description: Flight mode when Channel 5 pwm is >1360, <= 1490
// @Values: 0:Stabilize,1:Acro,2:AltHold,3:Auto,4:Guided,5:Loiter,6:RTL,7:Circle,9:Land,10:OF_Loiter,11:Drift,13:Sport
// @User: Standard
GSCALAR(flight_mode3, "FLTMODE3", FLIGHT_MODE_3),
// @Param: FLTMODE4
// @DisplayName: Flight Mode 4
// @Description: Flight mode when Channel 5 pwm is >1490, <= 1620
// @Values: 0:Stabilize,1:Acro,2:AltHold,3:Auto,4:Guided,5:Loiter,6:RTL,7:Circle,9:Land,10:OF_Loiter,11:Drift,13:Sport
// @User: Standard
GSCALAR(flight_mode4, "FLTMODE4", FLIGHT_MODE_4),
// @Param: FLTMODE5
// @DisplayName: Flight Mode 5
// @Description: Flight mode when Channel 5 pwm is >1620, <= 1749
// @Values: 0:Stabilize,1:Acro,2:AltHold,3:Auto,4:Guided,5:Loiter,6:RTL,7:Circle,9:Land,10:OF_Loiter,11:Drift,13:Sport
// @User: Standard
GSCALAR(flight_mode5, "FLTMODE5", FLIGHT_MODE_5),
// @Param: FLTMODE6
// @DisplayName: Flight Mode 6
// @Description: Flight mode when Channel 5 pwm is >=1750
// @Values: 0:Stabilize,1:Acro,2:AltHold,3:Auto,4:Guided,5:Loiter,6:RTL,7:Circle,9:Land,10:OF_Loiter,11:Drift,13:Sport
// @User: Standard
GSCALAR(flight_mode6, "FLTMODE6", FLIGHT_MODE_6),
// @Param: SIMPLE
// @DisplayName: Simple mode bitmask
// @Description: Bitmask which holds which flight modes use simple heading mode (eg bit 0 = 1 means Flight Mode 0 uses simple mode)
// @User: Advanced
GSCALAR(simple_modes, "SIMPLE", 0),
// @Param: LOG_BITMASK
// @DisplayName: Log bitmask
// @Description: 2 byte bitmap of log types to enable
// @Values: 830:Default,894:Default+RCIN,958:Default+IMU,1854:Default+Motors,-6146:NearlyAll,0:Disabled
// @User: Standard
GSCALAR(log_bitmask, "LOG_BITMASK", DEFAULT_LOG_BITMASK),
// @Param: ESC
// @DisplayName: ESC Calibration
// @Description: Controls whether ArduCopter will enter ESC calibration on the next restart. Do not adjust this parameter manually.
// @User: Advanced
// @Values: 0:Normal Start-up,1:Start-up in ESC Calibration mode
GSCALAR(esc_calibrate, "ESC", 0),
// @Param: TUNE
// @DisplayName: Channel 6 Tuning
// @Description: Controls which parameters (normally PID gains) are being tuned with transmitter's channel 6 knob
// @User: Standard
// @Values: 0:None,1:Stab Roll/Pitch kP,4:Rate Roll/Pitch kP,5:Rate Roll/Pitch kI,21:Rate Roll/Pitch kD,3:Stab Yaw kP,6:Rate Yaw kP,26:Rate Yaw kD,14:Altitude Hold kP,7:Throttle Rate kP,34:Throttle Accel kP,35:Throttle Accel kI,36:Throttle Accel kD,42:Loiter Speed,12:Loiter Pos kP,22:Loiter Rate kP,28:Loiter Rate kI,23:Loiter Rate kD,10:WP Speed,25:Acro RollPitch kP,40:Acro Yaw kP,9:Relay On/Off,13:Heli Ext Gyro,17:OF Loiter kP,18:OF Loiter kI,19:OF Loiter kD,30:AHRS Yaw kP,31:AHRS kP,32:INAV_TC,38:Declination,39:Circle Rate,41:Sonar Gain
GSCALAR(radio_tuning, "TUNE", 0),
// @Param: TUNE_LOW
// @DisplayName: Tuning minimum
// @Description: The minimum value that will be applied to the parameter currently being tuned with the transmitter's channel 6 knob
// @User: Standard
// @Range: 0 32767
GSCALAR(radio_tuning_low, "TUNE_LOW", 0),
// @Param: TUNE_HIGH
// @DisplayName: Tuning maximum
// @Description: The maximum value that will be applied to the parameter currently being tuned with the transmitter's channel 6 knob
// @User: Standard
// @Range: 0 32767
GSCALAR(radio_tuning_high, "TUNE_HIGH", 1000),
// @Param: FRAME
// @DisplayName: Frame Orientation (+, X or V)
// @Description: Controls motor mixing for multicopters. Not used for Tri or Traditional Helicopters.
// @Values: 0:Plus, 1:X, 2:V, 3:H, 10:Y6B (New)
// @User: Standard
GSCALAR(frame_orientation, "FRAME", AP_MOTORS_X_FRAME),
// @Param: CH7_OPT
// @DisplayName: Channel 7 option
// @Description: Select which function if performed when CH7 is above 1800 pwm
// @Values: 0:Do Nothing, 2:Flip, 3:Simple Mode, 4:RTL, 5:Save Trim, 7:Save WP, 8:Multi Mode, 9:Camera Trigger, 10:Sonar, 11:Fence, 12:ResetToArmedYaw, 13:Super Simple Mode, 14:Acro Trainer, 16:Auto, 17:AutoTune, 18:Land, 19:EPM
// @User: Standard
GSCALAR(ch7_option, "CH7_OPT", CH7_OPTION),
// @Param: CH8_OPT
// @DisplayName: Channel 8 option
// @Description: Select which function if performed when CH8 is above 1800 pwm
// @Values: 0:Do Nothing, 2:Flip, 3:Simple Mode, 4:RTL, 5:Save Trim, 7:Save WP, 8:Multi Mode, 9:Camera Trigger, 10:Sonar, 11:Fence, 12:ResetToArmedYaw, 13:Super Simple Mode, 14:Acro Trainer, 16:Auto, 17:AutoTune, 18:Land, 19:EPM
// @User: Standard
GSCALAR(ch8_option, "CH8_OPT", CH8_OPTION),
// @Param: ARMING_CHECK
// @DisplayName: Arming check
// @Description: Allows enabling or disabling of pre-arming checks of receiver, accelerometer, barometer, compass and GPS
// @Values: 0:Disabled, 1:Enabled, -3:Skip Baro, -5:Skip Compass, -9:Skip GPS, -17:Skip INS, -33:Skip Parameters, -65:Skip RC, 127:Skip Voltage
// @User: Standard
GSCALAR(arming_check, "ARMING_CHECK", ARMING_CHECK_ALL),
// @Param: ANGLE_MAX
// @DisplayName: Angle Max
// @Description: Maximum lean angle in all flight modes
// @Range 1000 8000
// @User: Advanced
ASCALAR(angle_max, "ANGLE_MAX", DEFAULT_ANGLE_MAX),
// @Param: RC_FEEL_RP
// @DisplayName: RC Feel Roll/Pitch
// @Description: RC feel for roll/pitch which controls vehicle response to user input with 0 being extremely soft and 100 begin crisp
// @User: Advanced
// @Values: 0:Very Soft, 25:Soft, 50:Medium, 75:Crisp, 100:Very Crisp
GSCALAR(rc_feel_rp, "RC_FEEL_RP", RC_FEEL_RP_VERY_CRISP),
#if FRAME_CONFIG == HELI_FRAME
// @Group: HS1_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(heli_servo_1, "HS1_", RC_Channel),
// @Group: HS2_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(heli_servo_2, "HS2_", RC_Channel),
// @Group: HS3_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(heli_servo_3, "HS3_", RC_Channel),
// @Group: HS4_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(heli_servo_4, "HS4_", RC_Channel),
// @Param: H_STAB_COL_MIN
// @DisplayName: Heli Stabilize Throttle Collective Minimum
// @Description: Helicopter's minimum collective position while pilot directly controls collective in stabilize mode
// @Range: 0 500
// @Units: Percent*10
// @Increment: 1
// @User: Standard
GSCALAR(heli_stab_col_min, "H_STAB_COL_MIN", HELI_STAB_COLLECTIVE_MIN_DEFAULT),
// @Param: H_STAB_COL_MAX
// @DisplayName: Stabilize Throttle Maximum
// @Description: Helicopter's maximum collective position while pilot directly controls collective in stabilize mode
// @Range: 500 1000
// @Units: Percent*10
// @Increment: 1
// @User: Standard
GSCALAR(heli_stab_col_max, "H_STAB_COL_MAX", HELI_STAB_COLLECTIVE_MAX_DEFAULT),
#endif
// RC channel
//-----------
// @Group: RC1_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(rc_1, "RC1_", RC_Channel),
// @Group: RC2_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(rc_2, "RC2_", RC_Channel),
// @Group: RC3_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(rc_3, "RC3_", RC_Channel),
// @Group: RC4_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(rc_4, "RC4_", RC_Channel),
// @Group: RC5_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_5, "RC5_", RC_Channel_aux),
// @Group: RC6_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_6, "RC6_", RC_Channel_aux),
// @Group: RC7_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_7, "RC7_", RC_Channel_aux),
// @Group: RC8_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_8, "RC8_", RC_Channel_aux),
#if CONFIG_HAL_BOARD == HAL_BOARD_PX4
// @Group: RC9_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_9, "RC9_", RC_Channel_aux),
#endif
// @Group: RC10_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_10, "RC10_", RC_Channel_aux),
// @Group: RC11_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_11, "RC11_", RC_Channel_aux),
#if CONFIG_HAL_BOARD == HAL_BOARD_PX4
// @Group: RC12_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_12, "RC12_", RC_Channel_aux),
#endif
// @Param: RC_SPEED
// @DisplayName: ESC Update Speed
// @Description: This is the speed in Hertz that your ESCs will receive updates
// @Units: Hz
// @Range: 50 490
// @Increment: 1
// @User: Advanced
GSCALAR(rc_speed, "RC_SPEED", RC_FAST_SPEED),
// @Param: ACRO_RP_P
// @DisplayName: Acro Roll and Pitch P gain
// @Description: Converts pilot roll and pitch into a desired rate of rotation in ACRO and SPORT mode. Higher values mean faster rate of rotation.
// @Range: 1 10
// @User: Standard
GSCALAR(acro_rp_p, "ACRO_RP_P", ACRO_RP_P),
// @Param: ACRO_YAW_P
// @DisplayName: Acro Yaw P gain
// @Description: Converts pilot yaw input into a desired rate of rotation in ACRO, Stabilize and SPORT modes. Higher values mean faster rate of rotation.
// @Range: 1 10
// @User: Standard
GSCALAR(acro_yaw_p, "ACRO_YAW_P", ACRO_YAW_P),
// @Param: ACRO_BAL_ROLL
// @DisplayName: Acro Balance Roll
// @Description: rate at which roll angle returns to level in acro mode
// @Range: 0 3
// @Increment: 0.1
// @User: Advanced
GSCALAR(acro_balance_roll, "ACRO_BAL_ROLL", ACRO_BALANCE_ROLL),
// @Param: ACRO_BAL_PITCH
// @DisplayName: Acro Balance Pitch
// @Description: rate at which pitch angle returns to level in acro mode
// @Range: 0 3
// @Increment: 0.1
// @User: Advanced
GSCALAR(acro_balance_pitch, "ACRO_BAL_PITCH", ACRO_BALANCE_PITCH),
// @Param: ACRO_TRAINER
// @DisplayName: Acro Trainer
// @Description: Type of trainer used in acro mode
// @Values: 0:Disabled,1:Leveling,2:Leveling and Limited
// @User: Advanced
GSCALAR(acro_trainer, "ACRO_TRAINER", ACRO_TRAINER_LIMITED),
// PID controller
//---------------
// @Param: RATE_RLL_P
// @DisplayName: Roll axis rate controller P gain
// @Description: Roll axis rate controller P gain. Converts the difference between desired roll rate and actual roll rate into a motor speed output
// @Range: 0.08 0.20
// @Increment: 0.005
// @User: Standard
// @Param: RATE_RLL_I
// @DisplayName: Roll axis rate controller I gain
// @Description: Roll axis rate controller I gain. Corrects long-term difference in desired roll rate vs actual roll rate
// @Range: 0.01 0.5
// @Increment: 0.01
// @User: Standard
// @Param: RATE_RLL_IMAX
// @DisplayName: Roll axis rate controller I gain maximum
// @Description: Roll axis rate controller I gain maximum. Constrains the maximum motor output that the I gain will output
// @Range: 0 500
// @Increment: 10
// @Units: Percent*10
// @User: Standard
// @Param: RATE_RLL_D
// @DisplayName: Roll axis rate controller D gain
// @Description: Roll axis rate controller D gain. Compensates for short-term change in desired roll rate vs actual roll rate
// @Range: 0.001 0.02
// @Increment: 0.001
// @User: Standard
GGROUP(pid_rate_roll, "RATE_RLL_", AC_PID),
// @Param: RATE_PIT_P
// @DisplayName: Pitch axis rate controller P gain
// @Description: Pitch axis rate controller P gain. Converts the difference between desired pitch rate and actual pitch rate into a motor speed output
// @Range: 0.08 0.20
// @Increment: 0.005
// @User: Standard
// @Param: RATE_PIT_I
// @DisplayName: Pitch axis rate controller I gain
// @Description: Pitch axis rate controller I gain. Corrects long-term difference in desired pitch rate vs actual pitch rate
// @Range: 0.01 0.5
// @Increment: 0.01
// @User: Standard
// @Param: RATE_PIT_IMAX
// @DisplayName: Pitch axis rate controller I gain maximum
// @Description: Pitch axis rate controller I gain maximum. Constrains the maximum motor output that the I gain will output
// @Range: 0 500
// @Increment: 10
// @Units: Percent*10
// @User: Standard
// @Param: RATE_PIT_D
// @DisplayName: Pitch axis rate controller D gain
// @Description: Pitch axis rate controller D gain. Compensates for short-term change in desired pitch rate vs actual pitch rate
// @Range: 0.001 0.02
// @Increment: 0.001
// @User: Standard
GGROUP(pid_rate_pitch, "RATE_PIT_", AC_PID),
// @Param: RATE_YAW_P
// @DisplayName: Yaw axis rate controller P gain
// @Description: Yaw axis rate controller P gain. Converts the difference between desired yaw rate and actual yaw rate into a motor speed output
// @Range: 0.150 0.250
// @Increment: 0.005
// @User: Standard
// @Param: RATE_YAW_I
// @DisplayName: Yaw axis rate controller I gain
// @Description: Yaw axis rate controller I gain. Corrects long-term difference in desired yaw rate vs actual yaw rate
// @Range: 0.010 0.020
// @Increment: 0.01
// @User: Standard
// @Param: RATE_YAW_IMAX
// @DisplayName: Yaw axis rate controller I gain maximum
// @Description: Yaw axis rate controller I gain maximum. Constrains the maximum motor output that the I gain will output
// @Range: 0 800
// @Increment: 10
// @Units: Percent*10
// @User: Standard
// @Param: RATE_YAW_D
// @DisplayName: Yaw axis rate controller D gain
// @Description: Yaw axis rate controller D gain. Compensates for short-term change in desired yaw rate vs actual yaw rate
// @Range: 0.000 0.02
// @Increment: 0.001
// @User: Standard
GGROUP(pid_rate_yaw, "RATE_YAW_", AC_PID),
// @Param: LOITER_LAT_P
// @DisplayName: Loiter latitude rate controller P gain
// @Description: Loiter latitude rate controller P gain. Converts the difference between desired speed and actual speed into a lean angle in the latitude direction
// @Range: 0.1 6.0
// @Increment: 0.1
// @User: Advanced
// @Param: LOITER_LAT_I
// @DisplayName: Loiter latitude rate controller I gain
// @Description: Loiter latitude rate controller I gain. Corrects long-term difference in desired speed and actual speed in the latitude direction
// @Range: 0.02 1.00
// @Increment: 0.01
// @User: Advanced
// @Param: LOITER_LAT_IMAX
// @DisplayName: Loiter rate controller I gain maximum
// @Description: Loiter rate controller I gain maximum. Constrains the lean angle that the I gain will output
// @Range: 0 4500
// @Increment: 10
// @Units: Centi-Degrees
// @User: Advanced
// @Param: LOITER_LAT_D
// @DisplayName: Loiter latitude rate controller D gain
// @Description: Loiter latitude rate controller D gain. Compensates for short-term change in desired speed vs actual speed
// @Range: 0.0 0.6
// @Increment: 0.01
// @User: Advanced
GGROUP(pid_loiter_rate_lat, "LOITER_LAT_", AC_PID),
// @Param: LOITER_LON_P
// @DisplayName: Loiter longitude rate controller P gain
// @Description: Loiter longitude rate controller P gain. Converts the difference between desired speed and actual speed into a lean angle in the longitude direction
// @Range: 0.1 6.0
// @Increment: 0.1
// @User: Advanced
// @Param: LOITER_LON_I
// @DisplayName: Loiter longitude rate controller I gain
// @Description: Loiter longitude rate controller I gain. Corrects long-term difference in desired speed and actual speed in the longitude direction
// @Range: 0.02 1.00
// @Increment: 0.01
// @User: Advanced
// @Param: LOITER_LON_IMAX
// @DisplayName: Loiter longitude rate controller I gain maximum
// @Description: Loiter longitude rate controller I gain maximum. Constrains the lean angle that the I gain will output
// @Range: 0 4500
// @Increment: 10
// @Units: Centi-Degrees
// @User: Advanced
// @Param: LOITER_LON_D
// @DisplayName: Loiter longituderate controller D gain
// @Description: Loiter longitude rate controller D gain. Compensates for short-term change in desired speed vs actual speed
// @Range: 0.0 0.6
// @Increment: 0.01
// @User: Advanced
GGROUP(pid_loiter_rate_lon, "LOITER_LON_", AC_PID),
// @Param: THR_RATE_P
// @DisplayName: Throttle rate controller P gain
// @Description: Throttle rate controller P gain. Converts the difference between desired vertical speed and actual speed into a desired acceleration that is passed to the throttle acceleration controller
// @Range: 1.000 8.000
// @User: Standard
// @Param: THR_RATE_I
// @DisplayName: Throttle rate controller I gain
// @Description: Throttle rate controller I gain. Corrects long-term difference in desired vertical speed and actual speed
// @Range: 0.000 0.100
// @User: Standard
// @Param: THR_RATE_IMAX
// @DisplayName: Throttle rate controller I gain maximum
// @Description: Throttle rate controller I gain maximum. Constrains the desired acceleration that the I gain will generate
// @Range: 0 500
// @Units: cm/s/s
// @User: Standard
// @Param: THR_RATE_D
// @DisplayName: Throttle rate controller D gain
// @Description: Throttle rate controller D gain. Compensates for short-term change in desired vertical speed vs actual speed
// @Range: 0.000 0.400
// @User: Standard
GGROUP(p_throttle_rate, "THR_RATE_", AC_P),
// @Param: THR_ACCEL_P
// @DisplayName: Throttle acceleration controller P gain
// @Description: Throttle acceleration controller P gain. Converts the difference between desired vertical acceleration and actual acceleration into a motor output
// @Range: 0.500 1.500
// @User: Standard
// @Param: THR_ACCEL_I
// @DisplayName: Throttle acceleration controller I gain
// @Description: Throttle acceleration controller I gain. Corrects long-term difference in desired vertical acceleration and actual acceleration
// @Range: 0.000 3.000
// @User: Standard
// @Param: THR_ACCEL_IMAX
// @DisplayName: Throttle acceleration controller I gain maximum
// @Description: Throttle acceleration controller I gain maximum. Constrains the maximum pwm that the I term will generate
// @Range: 0 500
// @Units: Percent*10
// @User: Standard
// @Param: THR_ACCEL_D
// @DisplayName: Throttle acceleration controller D gain
// @Description: Throttle acceleration controller D gain. Compensates for short-term change in desired vertical acceleration vs actual acceleration
// @Range: 0.000 0.400
// @User: Standard
GGROUP(pid_throttle_accel,"THR_ACCEL_", AC_PID),
// @Param: OF_RLL_P
// @DisplayName: Optical Flow based loiter controller roll axis P gain
// @Description: Optical Flow based loiter controller roll axis P gain. Converts the position error from the target point to a roll angle
// @Range: 2.000 3.000
// @User: Standard
// @Param: OF_RLL_I
// @DisplayName: Optical Flow based loiter controller roll axis I gain
// @Description: Optical Flow based loiter controller roll axis I gain. Corrects long-term position error by more persistently rolling left or right
// @Range: 0.250 0.750
// @User: Standard
// @Param: OF_RLL_IMAX
// @DisplayName: Optical Flow based loiter controller roll axis I gain maximum
// @Description: Optical Flow based loiter controller roll axis I gain maximum. Constrains the maximum roll angle that the I term will generate
// @Range: 0 4500
// @Units: Centi-Degrees
// @User: Standard
// @Param: OF_RLL_D
// @DisplayName: Optical Flow based loiter controller roll axis D gain
// @Description: Optical Flow based loiter controller roll axis D gain. Compensates for short-term change in speed in the roll direction
// @Range: 0.100 0.140
// @User: Standard
GGROUP(pid_optflow_roll, "OF_RLL_", AC_PID),
// @Param: OF_PIT_P
// @DisplayName: Optical Flow based loiter controller pitch axis P gain
// @Description: Optical Flow based loiter controller pitch axis P gain. Converts the position error from the target point to a pitch angle
// @Range: 2.000 3.000
// @User: Standard
// @Param: OF_PIT_I
// @DisplayName: Optical Flow based loiter controller pitch axis I gain
// @Description: Optical Flow based loiter controller pitch axis I gain. Corrects long-term position error by more persistently pitching left or right
// @Range: 0.250 0.750
// @User: Standard
// @Param: OF_PIT_IMAX
// @DisplayName: Optical Flow based loiter controller pitch axis I gain maximum
// @Description: Optical Flow based loiter controller pitch axis I gain maximum. Constrains the maximum pitch angle that the I term will generate
// @Range: 0 4500
// @Units: Centi-Degrees
// @User: Standard
// @Param: OF_PIT_D
// @DisplayName: Optical Flow based loiter controller pitch axis D gain
// @Description: Optical Flow based loiter controller pitch axis D gain. Compensates for short-term change in speed in the pitch direction
// @Range: 0.100 0.140
// @User: Standard
GGROUP(pid_optflow_pitch, "OF_PIT_", AC_PID),
// PI controller
//--------------
// @Param: STB_RLL_P
// @DisplayName: Roll axis stabilize controller P gain
// @Description: Roll axis stabilize (i.e. angle) controller P gain. Converts the error between the desired roll angle and actual angle to a desired roll rate
// @Range: 3.000 6.000
// @User: Standard
// @Param: STB_RLL_I
// @DisplayName: Roll axis stabilize controller I gain
// @Description: Roll axis stabilize (i.e. angle) controller I gain. Corrects for longer-term difference in desired roll angle and actual angle
// @Range: 0.000 0.100
// @User: Standard
// @Param: STB_RLL_IMAX
// @DisplayName: Roll axis stabilize controller I gain maximum
// @Description: Roll axis stabilize (i.e. angle) controller I gain maximum. Constrains the maximum roll rate that the I term will generate
// @Range: 0 4500
// @Units: Centi-Degrees/Sec
// @User: Standard
GGROUP(p_stabilize_roll, "STB_RLL_", AC_P),
// @Param: STB_PIT_P
// @DisplayName: Pitch axis stabilize controller P gain
// @Description: Pitch axis stabilize (i.e. angle) controller P gain. Converts the error between the desired pitch angle and actual angle to a desired pitch rate
// @Range: 3.000 6.000
// @User: Standard
GGROUP(p_stabilize_pitch, "STB_PIT_", AC_P),
// @Param: STB_YAW_P
// @DisplayName: Yaw axis stabilize controller P gain
// @Description: Yaw axis stabilize (i.e. angle) controller P gain. Converts the error between the desired yaw angle and actual angle to a desired yaw rate
// @Range: 3.000 6.000
// @User: Standard
GGROUP(p_stabilize_yaw, "STB_YAW_", AC_P),
// @Param: THR_ALT_P
// @DisplayName: Altitude controller P gain
// @Description: Altitude controller P gain. Converts the difference between the desired altitude and actual altitude into a climb or descent rate which is passed to the throttle rate controller
// @Range: 1.000 3.000
// @User: Standard
GGROUP(p_alt_hold, "THR_ALT_", AC_P),
// @Param: HLD_LAT_P
// @DisplayName: Loiter position controller P gain
// @Description: Loiter position controller P gain. Converts the distance (in the latitude direction) to the target location into a desired speed which is then passed to the loiter latitude rate controller
// @Range: 0.500 2.000
// @User: Standard
GGROUP(p_loiter_pos, "HLD_LAT_", AC_P),
// variables not in the g class which contain EEPROM saved variables
#if CAMERA == ENABLED
// @Group: CAM_
// @Path: ../libraries/AP_Camera/AP_Camera.cpp
GOBJECT(camera, "CAM_", AP_Camera),
#endif
// @Group: RELAY_
// @Path: ../libraries/AP_Relay/AP_Relay.cpp
GOBJECT(relay, "RELAY_", AP_Relay),
#if EPM_ENABLED == ENABLED
// @Group: EPM_
// @Path: ../libraries/AP_EPM/AP_EPM.cpp
GOBJECT(epm, "EPM_", AP_EPM),
#endif
// @Group: COMPASS_
// @Path: ../libraries/AP_Compass/Compass.cpp
GOBJECT(compass, "COMPASS_", Compass),
// @Group: INS_
// @Path: ../libraries/AP_InertialSensor/AP_InertialSensor.cpp
GOBJECT(ins, "INS_", AP_InertialSensor),
// @Group: INAV_
// @Path: ../libraries/AP_InertialNav/AP_InertialNav.cpp
GOBJECT(inertial_nav, "INAV_", AP_InertialNav),
// @Group: WPNAV_
// @Path: ../libraries/AC_WPNav/AC_WPNav.cpp
GOBJECT(wp_nav, "WPNAV_", AC_WPNav),
// @Group: WPNAV_
// @Path: ../libraries/AC_WPNav/AC_Circle.cpp
GOBJECT(circle_nav, "CIRCLE_", AC_Circle),
#if FRAME_CONFIG == HELI_FRAME
// @Group: ATCON_
// @Path: ../libraries/AC_AttitudeControl/AC_AttitudeControl_Heli.cpp
GOBJECT(attitude_control, "ATC_", AC_AttitudeControl_Heli),
#else
// @Group: ATCON_
// @Path: ../libraries/AC_AttitudeControl/AC_AttitudeControl.cpp
GOBJECT(attitude_control, "ATC_", AC_AttitudeControl),
#endif
// @Group: POSCON_
// @Path: ../libraries/AC_AttitudeControl/AC_PosControl.cpp
GOBJECT(pos_control, "POSCON_", AC_PosControl),
// @Group: SR0_
// @Path: GCS_Mavlink.pde
GOBJECTN(gcs[0], gcs0, "SR0_", GCS_MAVLINK),
// @Group: SR1_
// @Path: GCS_Mavlink.pde
GOBJECTN(gcs[1], gcs1, "SR1_", GCS_MAVLINK),
#if MAVLINK_COMM_NUM_BUFFERS > 2
// @Group: SR2_
// @Path: GCS_Mavlink.pde
GOBJECTN(gcs[2], gcs2, "SR2_", GCS_MAVLINK),
#endif
// @Group: AHRS_
// @Path: ../libraries/AP_AHRS/AP_AHRS.cpp
GOBJECT(ahrs, "AHRS_", AP_AHRS),
#if MOUNT == ENABLED
// @Group: MNT_
// @Path: ../libraries/AP_Mount/AP_Mount.cpp
GOBJECT(camera_mount, "MNT_", AP_Mount),
#endif
#if MOUNT2 == ENABLED
// @Group: MNT2_
// @Path: ../libraries/AP_Mount/AP_Mount.cpp
GOBJECT(camera_mount2, "MNT2_", AP_Mount),
#endif
// @Group: BATT_
// @Path: ../libraries/AP_BattMonitor/AP_BattMonitor.cpp
GOBJECT(battery, "BATT_", AP_BattMonitor),
// @Group: BRD_
// @Path: ../libraries/AP_BoardConfig/AP_BoardConfig.cpp
GOBJECT(BoardConfig, "BRD_", AP_BoardConfig),
#if SPRAYER == ENABLED
// @Group: SPRAYER_
// @Path: ../libraries/AC_Sprayer/AC_Sprayer.cpp
GOBJECT(sprayer, "SPRAY_", AC_Sprayer),
#endif
#if CONFIG_HAL_BOARD == HAL_BOARD_AVR_SITL
GOBJECT(sitl, "SIM_", SITL),
#endif
// @Group: GND_
// @Path: ../libraries/AP_Baro/AP_Baro.cpp
GOBJECT(barometer, "GND_", AP_Baro),
// @Group: SCHED_
// @Path: ../libraries/AP_Scheduler/AP_Scheduler.cpp
GOBJECT(scheduler, "SCHED_", AP_Scheduler),
#if AC_FENCE == ENABLED
// @Group: FENCE_
// @Path: ../libraries/AC_Fence/AC_Fence.cpp
GOBJECT(fence, "FENCE_", AC_Fence),
#endif
// @Group: GPSGLITCH_
// @Path: ../libraries/AP_GPS/AP_GPS_Glitch.cpp
GOBJECT(gps_glitch, "GPSGLITCH_", GPS_Glitch),
#if FRAME_CONFIG == HELI_FRAME
// @Group: H_
// @Path: ../libraries/AP_Motors/AP_MotorsHeli.cpp
GOBJECT(motors, "H_", AP_MotorsHeli),
#elif FRAME_CONFIG == SINGLE_FRAME
// @Group: SS1_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(single_servo_1, "SS1_", RC_Channel),
// @Group: SS2_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(single_servo_2, "SS2_", RC_Channel),
// @Group: SS3_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(single_servo_3, "SS3_", RC_Channel),
// @Group: SS4_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(single_servo_4, "SS4_", RC_Channel),
// @Group: MOT_
// @Path: ../libraries/AP_Motors/AP_MotorsSingle.cpp
GOBJECT(motors, "MOT_", AP_MotorsSingle),
#elif FRAME_CONFIG == COAX_FRAME
// @Group: SS1_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(single_servo_1, "SS1_", RC_Channel),
// @Group: SS2_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(single_servo_2, "SS2_", RC_Channel),
// @Group: MOT_