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ardupilot/ArduPlane/Parameters.h

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// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
#ifndef PARAMETERS_H
#define PARAMETERS_H
#include <AP_Common.h>
// Global parameter class.
//
class Parameters {
public:
/*
* The value of k_format_version determines whether the existing
* eeprom data is considered valid. You should only change this
* value under the following circumstances:
*
* 1) the meaning of an existing eeprom parameter changes
*
* 2) the value of an existing k_param_* enum value changes
*
* Adding a new parameter should _not_ require a change to
* k_format_version except under special circumstances. If you
* change it anyway then all ArduPlane users will need to reload all
* their parameters. We want that to be an extremely rare
* thing. Please do not just change it "just in case".
*
* To determine if a k_param_* value has changed, use the rules of
* C++ enums to work out the value of the neighboring enum
* values. If you don't know the C++ enum rules then please ask for
* help.
*/
//////////////////////////////////////////////////////////////////
// STOP!!! DO NOT CHANGE THIS VALUE UNTIL YOU FULLY UNDERSTAND THE
// COMMENTS ABOVE. IF UNSURE, ASK ANOTHER DEVELOPER!!!
static const uint16_t k_format_version = 13;
//////////////////////////////////////////////////////////////////
// The parameter software_type is set up solely for ground station use
// and identifies the software type (eg ArduPilotMega versus ArduCopterMega)
// GCS will interpret values 0-9 as ArduPilotMega. Developers may use
// values within that range to identify different branches.
//
static const uint16_t k_software_type = 0; // 0 for APM trunk
enum {
// Layout version number, always key zero.
//
k_param_format_version = 0,
k_param_software_type,
k_param_num_resets,
// Misc
//
k_param_auto_trim = 10,
k_param_log_bitmask,
k_param_pitch_trim_cd,
k_param_mix_mode,
k_param_reverse_elevons,
k_param_reverse_ch1_elevon,
k_param_reverse_ch2_elevon,
k_param_flap_1_percent,
k_param_flap_1_speed,
k_param_flap_2_percent,
k_param_flap_2_speed,
k_param_reset_switch_chan,
k_param_manual_level, // unused
k_param_land_pitch_cd,
k_param_ins_old, // *** Deprecated, remove with next eeprom number change
k_param_stick_mixing,
k_param_reset_mission_chan,
k_param_land_flare_alt,
k_param_land_flare_sec,
k_param_crosstrack_min_distance, // unused
k_param_rudder_steer, // unused
k_param_throttle_nudge,
k_param_alt_offset,
k_param_ins, // libraries/AP_InertialSensor variables
k_param_takeoff_throttle_min_speed,
k_param_takeoff_throttle_min_accel,
k_param_takeoff_heading_hold, // unused
k_param_level_roll_limit,
k_param_hil_servos,
k_param_vtail_output,
k_param_nav_controller,
k_param_elevon_output,
k_param_att_controller,
k_param_mixing_gain,
// 110: Telemetry control
//
k_param_gcs0 = 110, // stream rates for port0
k_param_gcs3, // stream rates for port3
k_param_sysid_this_mav,
k_param_sysid_my_gcs,
k_param_serial3_baud,
k_param_telem_delay,
k_param_serial0_baud,
// 120: Fly-by-wire control
//
k_param_flybywire_airspeed_min = 120,
k_param_flybywire_airspeed_max,
k_param_FBWB_min_altitude_cm, // 0=disabled, minimum value for altitude in cm (for first time try 30 meters = 3000 cm)
k_param_flybywire_elev_reverse,
k_param_alt_control_algorithm,
k_param_flybywire_climb_rate,
//
// 130: Sensor parameters
//
k_param_imu = 130, // unused
k_param_altitude_mix,
k_param_compass_enabled,
k_param_compass,
k_param_battery_monitoring,
k_param_volt_div_ratio,
k_param_curr_amp_per_volt,
k_param_input_voltage, // deprecated, can be deleted
k_param_pack_capacity,
k_param_sonar_enabled,
k_param_ahrs, // AHRS group
k_param_barometer, // barometer ground calibration
k_param_airspeed, // AP_Airspeed parameters
k_param_curr_amp_offset,
//
// 150: Navigation parameters
//
k_param_crosstrack_gain = 150, // unused
k_param_crosstrack_entry_angle, // unused
k_param_roll_limit_cd,
k_param_pitch_limit_max_cd,
k_param_pitch_limit_min_cd,
k_param_airspeed_cruise_cm,
k_param_RTL_altitude_cm,
k_param_inverted_flight_ch,
k_param_min_gndspeed_cm,
k_param_crosstrack_use_wind, // unused
//
// Camera and mount parameters
//
k_param_camera = 160,
k_param_camera_mount,
k_param_camera_mount2,
//
// Battery monitoring parameters
//
k_param_rssi_pin = 167,
k_param_battery_volt_pin,
k_param_battery_curr_pin, // 169
//
// 170: Radio settings
//
k_param_channel_roll = 170,
k_param_channel_pitch,
k_param_channel_throttle,
k_param_channel_rudder,
k_param_rc_5,
k_param_rc_6,
k_param_rc_7,
k_param_rc_8,
k_param_rc_9,
k_param_rc_10,
k_param_rc_11,
k_param_throttle_min,
k_param_throttle_max,
k_param_throttle_fs_enabled,
k_param_throttle_fs_value,
k_param_throttle_cruise,
k_param_short_fs_action,
k_param_long_fs_action,
k_param_gcs_heartbeat_fs_enabled,
k_param_throttle_slewrate,
k_param_throttle_suppress_manual,
k_param_throttle_passthru_stabilize,
k_param_rc_12,
k_param_fs_batt_voltage,
k_param_fs_batt_mah,
//
// 200: Feed-forward gains
//
k_param_kff_pitch_compensation = 200, // unused
k_param_kff_rudder_mix,
k_param_kff_pitch_to_throttle,
k_param_kff_throttle_to_pitch,
k_param_scaling_speed,
//
// 210: flight modes
//
k_param_flight_mode_channel = 210,
k_param_flight_mode1,
k_param_flight_mode2,
k_param_flight_mode3,
k_param_flight_mode4,
k_param_flight_mode5,
k_param_flight_mode6,
//
// 220: Waypoint data
//
k_param_waypoint_mode = 220,
k_param_command_total,
k_param_command_index,
k_param_waypoint_radius,
k_param_loiter_radius,
k_param_fence_action,
k_param_fence_total,
k_param_fence_channel,
k_param_fence_minalt,
k_param_fence_maxalt,
// other objects
k_param_sitl = 230,
k_param_obc,
k_param_rollController,
k_param_pitchController,
k_param_yawController,
k_param_L1_controller,
//
// 240: PID Controllers
k_param_pidNavRoll = 240, // unused
k_param_pidServoRoll, // unused
k_param_pidServoPitch, // unused
k_param_pidNavPitchAirspeed,
k_param_pidServoRudder,
k_param_pidTeThrottle,
k_param_pidNavPitchAltitude,
k_param_pidWheelSteer,
// 254,255: reserved
};
AP_Int16 format_version;
AP_Int8 software_type;
// Telemetry control
//
AP_Int16 sysid_this_mav;
AP_Int16 sysid_my_gcs;
AP_Int8 serial0_baud;
AP_Int8 serial3_baud;
AP_Int8 telem_delay;
// Feed-forward gains
//
AP_Float kff_rudder_mix;
AP_Float kff_pitch_to_throttle;
AP_Float kff_throttle_to_pitch;
// speed used for speed scaling
AP_Float scaling_speed;
// navigation controller type. See AP_Navigation::ControllerType
AP_Int8 nav_controller;
// Estimation
//
AP_Float altitude_mix;
AP_Int8 alt_control_algorithm;
// Waypoints
//
AP_Int8 waypoint_mode;
AP_Int8 command_total;
AP_Int8 command_index;
AP_Int16 waypoint_radius;
AP_Int16 loiter_radius;
#if GEOFENCE_ENABLED == ENABLED
AP_Int8 fence_action;
AP_Int8 fence_total;
AP_Int8 fence_channel;
AP_Int16 fence_minalt; // meters
AP_Int16 fence_maxalt; // meters
#endif
// Fly-by-wire
//
AP_Int16 flybywire_airspeed_min;
AP_Int16 flybywire_airspeed_max;
AP_Int8 flybywire_elev_reverse;
AP_Int8 flybywire_climb_rate;
// Throttle
//
AP_Int8 throttle_min;
AP_Int8 throttle_max;
AP_Int8 throttle_slewrate;
AP_Int8 throttle_suppress_manual;
AP_Int8 throttle_passthru_stabilize;
AP_Int8 throttle_fs_enabled;
AP_Int16 throttle_fs_value;
AP_Int8 throttle_cruise;
AP_Int8 throttle_nudge;
// Failsafe
AP_Int8 short_fs_action;
AP_Int8 long_fs_action;
AP_Int8 gcs_heartbeat_fs_enabled;
AP_Float fs_batt_voltage;
AP_Float fs_batt_mah;
// Flight modes
//
AP_Int8 flight_mode_channel;
AP_Int8 flight_mode1;
AP_Int8 flight_mode2;
AP_Int8 flight_mode3;
AP_Int8 flight_mode4;
AP_Int8 flight_mode5;
AP_Int8 flight_mode6;
// Navigational maneuvering limits
//
AP_Int16 roll_limit_cd;
AP_Int16 pitch_limit_max_cd;
AP_Int16 pitch_limit_min_cd;
AP_Int16 alt_offset;
// Misc
//
AP_Int8 auto_trim;
AP_Int8 mix_mode;
AP_Int8 vtail_output;
AP_Int8 elevon_output;
AP_Float mixing_gain;
AP_Int8 reverse_elevons;
AP_Int8 reverse_ch1_elevon;
AP_Int8 reverse_ch2_elevon;
AP_Int16 num_resets;
AP_Int16 log_bitmask;
AP_Int8 reset_switch_chan;
AP_Int8 reset_mission_chan;
AP_Int32 airspeed_cruise_cm;
AP_Int32 RTL_altitude_cm;
AP_Int16 land_pitch_cd;
AP_Float land_flare_alt;
AP_Float land_flare_sec;
AP_Int32 min_gndspeed_cm;
AP_Int16 pitch_trim_cd;
AP_Int16 FBWB_min_altitude_cm;
#if HIL_MODE != HIL_MODE_DISABLED
AP_Int8 hil_servos;
#endif
AP_Int8 compass_enabled;
AP_Int8 battery_monitoring; // 0=disabled, 3=voltage only, 4=voltage and current
AP_Int8 flap_1_percent;
AP_Int8 flap_1_speed;
AP_Int8 flap_2_percent;
AP_Int8 flap_2_speed;
AP_Float volt_div_ratio;
AP_Float curr_amp_per_volt;
AP_Float curr_amp_offset;
AP_Int32 pack_capacity; // Battery pack capacity less reserve
AP_Int8 rssi_pin;
AP_Int8 battery_volt_pin;
AP_Int8 battery_curr_pin;
AP_Int8 inverted_flight_ch; // 0=disabled, 1-8 is channel for inverted flight trigger
AP_Int8 stick_mixing;
AP_Float takeoff_throttle_min_speed;
AP_Float takeoff_throttle_min_accel;
AP_Int8 level_roll_limit;
// RC channels
RC_Channel channel_roll;
RC_Channel channel_pitch;
RC_Channel channel_throttle;
RC_Channel channel_rudder;
RC_Channel_aux rc_5;
RC_Channel_aux rc_6;
RC_Channel_aux rc_7;
RC_Channel_aux rc_8;
#if CONFIG_HAL_BOARD == HAL_BOARD_APM2 || CONFIG_HAL_BOARD == HAL_BOARD_PX4
RC_Channel_aux rc_9;
RC_Channel_aux rc_10;
RC_Channel_aux rc_11;
#endif
#if CONFIG_HAL_BOARD == HAL_BOARD_PX4
RC_Channel_aux rc_12;
#endif
// Attitude to servo controllers
//
AP_RollController rollController;
AP_PitchController pitchController;
AP_YawController yawController;
// PID controllers
PID pidNavPitchAirspeed;
PID pidTeThrottle;
PID pidNavPitchAltitude;
PID pidWheelSteer;
Parameters() :
// variable default
//----------------------------------------
channel_roll (CH_1),
channel_pitch (CH_2),
channel_throttle (CH_3),
channel_rudder (CH_4),
rc_5 (CH_5),
rc_6 (CH_6),
rc_7 (CH_7),
rc_8 (CH_8),
#if CONFIG_HAL_BOARD == HAL_BOARD_APM2 || CONFIG_HAL_BOARD == HAL_BOARD_PX4
rc_9 (CH_9),
rc_10 (CH_10),
rc_11 (CH_11),
#endif
#if CONFIG_HAL_BOARD == HAL_BOARD_PX4
rc_12 (CH_12),
#endif
// PID controller initial P initial I initial D initial imax
//-----------------------------------------------------------------------------------
pidNavPitchAirspeed (NAV_PITCH_ASP_P, NAV_PITCH_ASP_I, NAV_PITCH_ASP_D, NAV_PITCH_ASP_INT_MAX_CMSEC),
pidTeThrottle (THROTTLE_TE_P, THROTTLE_TE_I, THROTTLE_TE_D, THROTTLE_TE_INT_MAX),
pidNavPitchAltitude (NAV_PITCH_ALT_P, NAV_PITCH_ALT_I, NAV_PITCH_ALT_D, NAV_PITCH_ALT_INT_MAX_CM),
pidWheelSteer (0, 0, 0, 0)
{}
};
extern const AP_Param::Info var_info[];
#endif // PARAMETERS_H
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