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ardupilot/ArduCopter/Parameters.h

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updated Param gen - won't compile yet. git-svn-id: https://arducopter.googlecode.com/svn/trunk@1666 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-02-17 03:09:13 -04:00
// -*- 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:
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
// The version of the layout as described by the parameter enum.
//
// When changing the parameter enum in an incompatible fashion, this
// value should be incremented by one.
//
// The increment will prevent old parameters from being used incorrectly
// by newer code.
//
Upped version added new logging params added crosstrack gain re-ordered param inits
2011-11-19 18:00:23 -04:00
static const uint16_t k_format_version = 113;
AC2.0.24b git-svn-id: https://arducopter.googlecode.com/svn/trunk@2567 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-06-16 14:03:26 -03:00
// The parameter software_type is set up solely for ground station use
// and identifies the software type (eg ArduPilotMega versus ArduCopterMega)
renamed some command variables to align with Arduplane reworked the arming code and moved the DCM gains out. updated climb_rate to include sonar data.
2011-11-05 01:41:51 -03:00
// GCS will interpret values 0-9 as ArduPilotMega. Developers may use
AC2.0.24b git-svn-id: https://arducopter.googlecode.com/svn/trunk@2567 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-06-16 14:03:26 -03:00
// values within that range to identify different branches.
//
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
static const uint16_t k_software_type = 10; // 0 for APM trunk
//
// Parameter identities.
//
// The enumeration defined here is used to ensure that every parameter
// or parameter group has a unique ID number. This number is used by
// AP_Var to store and locate parameters in EEPROM.
//
// Note that entries without a number are assigned the next number after
// the entry preceding them. When adding new entries, ensure that they
// don't overlap.
//
// Try to group related variables together, and assign them a set
// range in the enumeration. Place these groups in numerical order
// at the end of the enumeration.
//
// WARNING: Care should be taken when editing this enumeration as the
// AP_Var load/save code depends on the values here to identify
// variables saved in EEPROM.
//
//
enum {
// Layout version number, always key zero.
//
k_param_format_version = 0,
k_param_software_type,
// Misc
//
Upped version added new logging params added crosstrack gain re-ordered param inits
2011-11-19 18:00:23 -04:00
k_param_log_bitmask = 20,
k_param_log_last_filenumber,
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
TradHeli - added servo averaging to allow support of analog servos - moved heli parameters to 80 because they were causing flight modes to overlap with waypoints
2011-09-25 04:51:25 -03:00
#if FRAME_CONFIG == HELI_FRAME
//
// 80: Heli
//
k_param_heli_servo_1 = 80,
k_param_heli_servo_2,
k_param_heli_servo_3,
k_param_heli_servo_4,
k_param_heli_servo1_pos ,
k_param_heli_servo2_pos,
k_param_heli_servo3_pos,
k_param_heli_roll_max,
k_param_heli_pitch_max,
k_param_heli_collective_min,
k_param_heli_collective_max,
k_param_heli_collective_mid,
k_param_heli_ext_gyro_enabled,
k_param_heli_ext_gyro_gain,
TradHeli - new parameter HSV_MAN to allow better set-up from APMissionPlanner. Also changed swash movement to use radio_out which fixes some setup bugs
2011-11-12 10:23:07 -04:00
k_param_heli_servo_averaging,
TradHeli - added two parameters to improve heli control. heli_phase_angle allows pilot roll/pitch command to be translated into mixed roll and pitch. heli_coll_yaw_effect mixes some collective into the yaw so tail can counter act collective movements more easily.
2011-11-13 09:20:57 -04:00
k_param_heli_servo_manual,
Mission Scripting updates
2011-11-16 04:19:29 -04:00
k_param_heli_phase_angle,
TradHeli - added two parameters to improve heli control. heli_phase_angle allows pilot roll/pitch command to be translated into mixed roll and pitch. heli_coll_yaw_effect mixes some collective into the yaw so tail can counter act collective movements more easily.
2011-11-13 09:20:57 -04:00
k_param_heli_coll_yaw_effect, // 97
TradHeli - added servo averaging to allow support of analog servos - moved heli parameters to 80 because they were causing flight modes to overlap with waypoints
2011-09-25 04:51:25 -03:00
#endif
Revved the firmware to force resetting the EERPOM
2011-09-25 16:24:02 -03:00
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
// 110: Telemetry control
//
k_param_streamrates_port0 = 110,
k_param_streamrates_port3,
k_param_sysid_this_mav,
k_param_sysid_my_gcs,
added SERIAL3_BAUD parameter this is the real baud rate divided by 1000. So 57600 is set as 57 git-svn-id: https://arducopter.googlecode.com/svn/trunk@2997 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-08-01 08:39:17 -03:00
k_param_serial3_baud,
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
//
// 140: Sensor parameters
//
k_param_IMU_calibration = 140,
k_param_battery_monitoring,
k_param_pack_capacity,
k_param_compass_enabled,
k_param_compass,
k_param_sonar,
k_param_frame_orientation,
k_param_top_bottom_ratio,
ACM - partial integration of optical flow sensor git-svn-id: https://arducopter.googlecode.com/svn/trunk@2934 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-21 20:14:53 -03:00
k_param_optflow_enabled,
Added Input Voltage value to params
2011-09-10 22:44:56 -03:00
k_param_input_voltage,
Added low voltage code flashing code.
2011-09-16 22:56:51 -03:00
k_param_low_voltage,
allow CH7 to be set via params
2011-11-26 17:19:11 -04:00
k_param_ch7_option,
Arducopter, RangeFinder - added SONAR_TYPE parameter and properly support the XL (default), LV and long distance XL (aka XLL) sonar types
2011-12-11 03:40:59 -04:00
k_param_sonar_type, // 153
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
//
// 160: Navigation parameters
//
Upped version added new logging params added crosstrack gain re-ordered param inits
2011-11-19 18:00:23 -04:00
k_param_RTL_altitude = 160,
k_param_crosstrack_gain,
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
//
// 180: Radio settings
//
k_param_rc_1 = 180,
k_param_rc_2,
k_param_rc_3,
k_param_rc_4,
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_throttle_min,
k_param_throttle_max,
k_param_throttle_fs_enabled,
k_param_throttle_fs_action,
k_param_throttle_fs_value,
k_param_throttle_cruise,
k_param_esc_calibrate,
Fixes Alt hold mistake Moves tuning into runtime definable param Added more IMax to throttle Signed-off-by: Jason Short <jasonshort@gmail.com>
2011-09-10 19:16:51 -03:00
k_param_radio_tuning,
Added gains to adjust travel of camera.
2011-10-15 20:34:57 -03:00
k_param_camera_pitch_gain,
k_param_camera_roll_gain,
2.0.35 Added camera reversing parameters in AP_Var Added RTL Throttle Hold set/check Added dynamic speed control to slow down as you reach waypoints and RTL Home upped Yaw Dead zone slightly. git-svn-id: https://arducopter.googlecode.com/svn/trunk@2841 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-12 17:04:15 -03:00
allow flight modes to be setup over MAVLink this adopts the same method of setting up flight modes over MAVLink as APM now has git-svn-id: https://arducopter.googlecode.com/svn/trunk@2885 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-17 07:30:53 -03:00
//
// 210: flight modes
//
k_param_flight_mode1,
k_param_flight_mode2,
k_param_flight_mode3,
k_param_flight_mode4,
k_param_flight_mode5,
k_param_flight_mode6,
Removed Simple Mode Added Simple option to mode switch positions removed unused OptFlow code added reset lat and lon error removed unused init_auto Fixed log formatting Added simple mode bitmask removed pitchmax added CLI setup for enabling Simple mode to any switch position
2011-09-14 17:58:18 -03:00
k_param_simple_modes,
allow flight modes to be setup over MAVLink this adopts the same method of setting up flight modes over MAVLink as APM now has git-svn-id: https://arducopter.googlecode.com/svn/trunk@2885 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-17 07:30:53 -03:00
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
//
// 220: Waypoint data
//
k_param_waypoint_mode = 220,
renamed some command variables to align with Arduplane reworked the arming code and moved the DCM gains out. updated climb_rate to include sonar data.
2011-11-05 01:41:51 -03:00
k_param_command_total,
k_param_command_index,
Mission Scripting updates
2011-11-16 04:19:29 -04:00
k_param_command_nav_index,
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
k_param_waypoint_radius,
k_param_loiter_radius,
k_param_waypoint_speed_max,
//
2.0.40 git-svn-id: https://arducopter.googlecode.com/svn/trunk@3252 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-09-04 21:15:36 -03:00
// 240: PI/D Controllers
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
//
Added Acro Params Allows user's to fly separate PI loops settings for Acro
2011-10-27 15:52:00 -03:00
k_param_pi_rate_roll = 235,
2.0.40 git-svn-id: https://arducopter.googlecode.com/svn/trunk@3252 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-09-04 21:15:36 -03:00
k_param_pi_rate_pitch,
k_param_pi_rate_yaw,
k_param_pi_stabilize_roll,
k_param_pi_stabilize_pitch,
k_param_pi_stabilize_yaw,
k_param_pi_loiter_lat,
k_param_pi_loiter_lon,
k_param_pi_nav_lat,
k_param_pi_nav_lon,
Added second PI loop for alt hold. Upped gains for default JDrones Frame added gains for second PI loop for alt removed some tests for 1280 space constraints
2011-10-02 15:36:23 -03:00
k_param_pi_alt_hold,
2.0.40 git-svn-id: https://arducopter.googlecode.com/svn/trunk@3252 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-09-04 21:15:36 -03:00
k_param_pi_throttle,
Added Acro Params Allows user's to fly separate PI loops settings for Acro
2011-10-27 15:52:00 -03:00
k_param_pi_acro_roll,
k_param_pi_acro_pitch,
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
increase firmware version this avoids problems with previously corrupted EEPROMs git-svn-id: https://arducopter.googlecode.com/svn/trunk@3235 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-09-04 03:42:36 -03:00
// 254,255: reserved
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
};
AP_Int16 format_version;
AC2.0.24b git-svn-id: https://arducopter.googlecode.com/svn/trunk@2567 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-06-16 14:03:26 -03:00
AP_Int8 software_type;
// Telemetry control
//
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
AP_Int16 sysid_this_mav;
AP_Int16 sysid_my_gcs;
Removed Simple Mode Added Simple option to mode switch positions removed unused OptFlow code added reset lat and lon error removed unused init_auto Fixed log formatting Added simple mode bitmask removed pitchmax added CLI setup for enabling Simple mode to any switch position
2011-09-14 17:58:18 -03:00
AP_Int8 serial3_baud;
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
Upped version added new logging params added crosstrack gain re-ordered param inits
2011-11-19 18:00:23 -04:00
AP_Int16 RTL_altitude;
AP_Int8 sonar_enabled;
Arducopter, RangeFinder - added SONAR_TYPE parameter and properly support the XL (default), LV and long distance XL (aka XLL) sonar types
2011-12-11 03:40:59 -04:00
AP_Int8 sonar_type; // 0 = XL, 1 = LV, 2 = XLL (XL with 10m range)
Upped version added new logging params added crosstrack gain re-ordered param inits
2011-11-19 18:00:23 -04:00
AP_Int8 battery_monitoring; // 0=disabled, 1=3 cell lipo, 2=4 cell lipo, 3=total voltage only, 4=total voltage and current
AP_Int16 pack_capacity; // Battery pack capacity less reserve
AP_Int8 compass_enabled;
AP_Int8 optflow_enabled;
AP_Float input_voltage;
AP_Float low_voltage;
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
// Waypoints
//
AP_Int8 waypoint_mode;
renamed some command variables to align with Arduplane reworked the arming code and moved the DCM gains out. updated climb_rate to include sonar data.
2011-11-05 01:41:51 -03:00
AP_Int8 command_total;
AP_Int8 command_index;
Mission Scripting updates
2011-11-16 04:19:29 -04:00
AP_Int8 command_nav_index;
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
AP_Int8 waypoint_radius;
Fixed type error in params
2011-11-12 19:15:33 -04:00
AP_Int16 loiter_radius;
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
AP_Int16 waypoint_speed_max;
Upped version added new logging params added crosstrack gain re-ordered param inits
2011-11-19 18:00:23 -04:00
AP_Float crosstrack_gain;
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
// Throttle
//
AP_Int16 throttle_min;
AP_Int16 throttle_max;
AP_Int8 throttle_fs_enabled;
AP_Int8 throttle_fs_action;
AP_Int16 throttle_fs_value;
AP_Int16 throttle_cruise;
// Flight modes
//
allow flight modes to be setup over MAVLink this adopts the same method of setting up flight modes over MAVLink as APM now has git-svn-id: https://arducopter.googlecode.com/svn/trunk@2885 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-17 07:30:53 -03:00
AP_Int8 flight_mode1;
AP_Int8 flight_mode2;
AP_Int8 flight_mode3;
AP_Int8 flight_mode4;
AP_Int8 flight_mode5;
AP_Int8 flight_mode6;
Removed Simple Mode Added Simple option to mode switch positions removed unused OptFlow code added reset lat and lon error removed unused init_auto Fixed log formatting Added simple mode bitmask removed pitchmax added CLI setup for enabling Simple mode to any switch position
2011-09-14 17:58:18 -03:00
AP_Int8 simple_modes;
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
// Misc
//
AP_Int16 log_bitmask;
Upped version added new logging params added crosstrack gain re-ordered param inits
2011-11-19 18:00:23 -04:00
AP_Int16 log_last_filenumber;
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
new ESC calibration routine git-svn-id: https://arducopter.googlecode.com/svn/trunk@2121 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-05-06 19:46:57 -03:00
AP_Int8 esc_calibrate;
Fixes Alt hold mistake Moves tuning into runtime definable param Added more IMax to throttle Signed-off-by: Jason Short <jasonshort@gmail.com>
2011-09-10 19:16:51 -03:00
AP_Int8 radio_tuning;
2.0.6 Beta updates. Frame options + X moved to AP_Var. Updated nav code. git-svn-id: https://arducopter.googlecode.com/svn/trunk@2345 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-05-18 20:38:24 -03:00
AP_Int8 frame_orientation;
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
AP_Float top_bottom_ratio;
allow CH7 to be set via params
2011-11-26 17:19:11 -04:00
AP_Int8 ch7_option;
Upped version added new logging params added crosstrack gain re-ordered param inits
2011-11-19 18:00:23 -04:00
updated Param gen - won't compile yet. git-svn-id: https://arducopter.googlecode.com/svn/trunk@1666 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-02-17 03:09:13 -04:00
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
#if FRAME_CONFIG == HELI_FRAME
Traditional Heli - merged heli code into ACM trunk code! git-svn-id: https://arducopter.googlecode.com/svn/trunk@2548 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-06-12 09:14:10 -03:00
// Heli
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
RC_Channel heli_servo_1, heli_servo_2, heli_servo_3, heli_servo_4; // servos for swash plate and tail
TradHeli - added two parameters to improve heli control. heli_phase_angle allows pilot roll/pitch command to be translated into mixed roll and pitch. heli_coll_yaw_effect mixes some collective into the yaw so tail can counter act collective movements more easily.
2011-11-13 09:20:57 -04:00
AP_Int16 heli_servo1_pos, heli_servo2_pos, heli_servo3_pos; // servo positions (3 because we don't need pos for tail servo)
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
AP_Int16 heli_roll_max, heli_pitch_max; // maximum allowed roll and pitch of swashplate
AP_Int16 heli_coll_min, heli_coll_max, heli_coll_mid; // min and max collective. mid = main blades at zero pitch
AP_Int8 heli_ext_gyro_enabled; // 0 = no external tail gyro, 1 = external tail gyro
TradHeli - added servo averaging to allow support of analog servos - moved heli parameters to 80 because they were causing flight modes to overlap with waypoints
2011-09-25 04:51:25 -03:00
AP_Int16 heli_ext_gyro_gain; // radio output 1000~2000 (value output on CH_7)
AP_Int8 heli_servo_averaging; // 0 or 1 = no averaging (250hz) for **digital servos**, 2=average of two samples (125hz), 3=three samples (83.3hz) **analog servos**, 4=four samples (62.5hz), 5=5 samples(50hz)
TradHeli - new parameter HSV_MAN to allow better set-up from APMissionPlanner. Also changed swash movement to use radio_out which fixes some setup bugs
2011-11-12 10:23:07 -04:00
AP_Int8 heli_servo_manual; // 0 = normal mode, 1 = radio inputs directly control swash. required for swash set-up
TradHeli - added two parameters to improve heli control. heli_phase_angle allows pilot roll/pitch command to be translated into mixed roll and pitch. heli_coll_yaw_effect mixes some collective into the yaw so tail can counter act collective movements more easily.
2011-11-13 09:20:57 -04:00
AP_Int16 heli_phase_angle; // 0 to 360 degrees. specifies mixing between roll and pitch for helis
Mission Scripting updates
2011-11-16 04:19:29 -04:00
AP_Float heli_coll_yaw_effect; // -5.0 ~ 5.0. Feed forward control from collective to yaw. 1.0 = move rudder right 1% for every 1% of collective above the mid point
AC2.0.24b git-svn-id: https://arducopter.googlecode.com/svn/trunk@2567 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-06-16 14:03:26 -03:00
#endif
2.0.40 git-svn-id: https://arducopter.googlecode.com/svn/trunk@3252 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-09-04 21:15:36 -03:00
// RC channels
updated Param gen - won't compile yet. git-svn-id: https://arducopter.googlecode.com/svn/trunk@1666 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-02-17 03:09:13 -04:00
RC_Channel rc_1;
RC_Channel rc_2;
RC_Channel rc_3;
RC_Channel rc_4;
RC_Channel rc_5;
RC_Channel rc_6;
RC_Channel rc_7;
Compilation fixes per request git-svn-id: https://arducopter.googlecode.com/svn/trunk@1671 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-02-17 05:36:33 -04:00
RC_Channel rc_8;
updated Param gen - won't compile yet. git-svn-id: https://arducopter.googlecode.com/svn/trunk@1666 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-02-17 03:09:13 -04:00
RC_Channel rc_camera_pitch;
RC_Channel rc_camera_roll;
Upped version added new logging params added crosstrack gain re-ordered param inits
2011-11-19 18:00:23 -04:00
Added gains to adjust travel of camera.
2011-10-15 20:34:57 -03:00
AP_Float camera_pitch_gain;
AP_Float camera_roll_gain;
updated Param gen - won't compile yet. git-svn-id: https://arducopter.googlecode.com/svn/trunk@1666 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-02-17 03:09:13 -04:00
2.0.40 git-svn-id: https://arducopter.googlecode.com/svn/trunk@3252 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-09-04 21:15:36 -03:00
// PI/D controllers
APM_PI pi_rate_roll;
APM_PI pi_rate_pitch;
APM_PI pi_rate_yaw;
APM_PI pi_stabilize_roll;
APM_PI pi_stabilize_pitch;
APM_PI pi_stabilize_yaw;
APM_PI pi_loiter_lat;
APM_PI pi_loiter_lon;
APM_PI pi_nav_lat;
APM_PI pi_nav_lon;
Added second PI loop for alt hold. Upped gains for default JDrones Frame added gains for second PI loop for alt removed some tests for 1280 space constraints
2011-10-02 15:36:23 -03:00
APM_PI pi_alt_hold;
2.0.40 git-svn-id: https://arducopter.googlecode.com/svn/trunk@3252 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-09-04 21:15:36 -03:00
APM_PI pi_throttle;
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
Added Acro Params Allows user's to fly separate PI loops settings for Acro
2011-10-27 15:52:00 -03:00
APM_PI pi_acro_roll;
APM_PI pi_acro_pitch;
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
uint8_t junk;
// Note: keep initializers here in the same order as they are declared above.
Parameters() :
// variable default key name
//-------------------------------------------------------------------------------------------------------------------
format_version (k_format_version, k_param_format_version, PSTR("SYSID_SW_MREV")),
software_type (k_software_type, k_param_software_type, PSTR("SYSID_SW_TYPE")),
sysid_this_mav (MAV_SYSTEM_ID, k_param_sysid_this_mav, PSTR("SYSID_THISMAV")),
sysid_my_gcs (255, k_param_sysid_my_gcs, PSTR("SYSID_MYGCS")),
added SERIAL3_BAUD parameter this is the real baud rate divided by 1000. So 57600 is set as 57 git-svn-id: https://arducopter.googlecode.com/svn/trunk@2997 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-08-01 08:39:17 -03:00
serial3_baud (SERIAL3_BAUD/1000, k_param_serial3_baud, PSTR("SERIAL3_BAUD")),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
Upped version added new logging params added crosstrack gain re-ordered param inits
2011-11-19 18:00:23 -04:00
RTL_altitude (ALT_HOLD_HOME * 100, k_param_RTL_altitude, PSTR("ALT_HOLD_RTL")),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
sonar_enabled (DISABLED, k_param_sonar, PSTR("SONAR_ENABLE")),
Arducopter, RangeFinder - added SONAR_TYPE parameter and properly support the XL (default), LV and long distance XL (aka XLL) sonar types
2011-12-11 03:40:59 -04:00
sonar_type (AP_RANGEFINDER_MAXSONARXL, k_param_sonar_type, PSTR("SONAR_TYPE")),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
battery_monitoring (DISABLED, k_param_battery_monitoring, PSTR("BATT_MONITOR")),
pack_capacity (HIGH_DISCHARGE, k_param_pack_capacity, PSTR("BATT_CAPACITY")),
compass_enabled (MAGNETOMETER, k_param_compass_enabled, PSTR("MAG_ENABLE")),
ACM - partial integration of optical flow sensor git-svn-id: https://arducopter.googlecode.com/svn/trunk@2934 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-21 20:14:53 -03:00
optflow_enabled (OPTFLOW, k_param_optflow_enabled, PSTR("FLOW_ENABLE")),
Added Input Voltage value to params
2011-09-10 22:44:56 -03:00
input_voltage (INPUT_VOLTAGE, k_param_input_voltage, PSTR("IN_VOLT")),
Added low voltage code flashing code.
2011-09-16 22:56:51 -03:00
low_voltage (LOW_VOLTAGE, k_param_low_voltage, PSTR("LOW_VOLT")),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
waypoint_mode (0, k_param_waypoint_mode, PSTR("WP_MODE")),
renamed some command variables to align with Arduplane reworked the arming code and moved the DCM gains out. updated climb_rate to include sonar data.
2011-11-05 01:41:51 -03:00
command_total (0, k_param_command_total, PSTR("WP_TOTAL")),
command_index (0, k_param_command_index, PSTR("WP_INDEX")),
Mission Scripting updates
2011-11-16 04:19:29 -04:00
command_nav_index (0, k_param_command_nav_index, PSTR("WP_MUST_INDEX")),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
waypoint_radius (WP_RADIUS_DEFAULT, k_param_waypoint_radius, PSTR("WP_RADIUS")),
Made loiter rad smaller in storage
2011-11-20 04:22:20 -04:00
loiter_radius (LOITER_RADIUS, k_param_loiter_radius, PSTR("WP_LOITER_RAD")),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
waypoint_speed_max (WAYPOINT_SPEED_MAX, k_param_waypoint_speed_max, PSTR("WP_SPEED_MAX")),
Upped version added new logging params added crosstrack gain re-ordered param inits
2011-11-19 18:00:23 -04:00
crosstrack_gain (CROSSTRACK_GAIN, k_param_crosstrack_gain, PSTR("XTRK_GAIN_SC")),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
throttle_min (0, k_param_throttle_min, PSTR("THR_MIN")),
throttle_max (1000, k_param_throttle_max, PSTR("THR_MAX")),
throttle_fs_enabled (THROTTLE_FAILSAFE, k_param_throttle_fs_enabled, PSTR("THR_FAILSAFE")),
throttle_fs_action (THROTTLE_FAILSAFE_ACTION, k_param_throttle_fs_action, PSTR("THR_FS_ACTION")),
throttle_fs_value (THROTTLE_FS_VALUE, k_param_throttle_fs_value, PSTR("THR_FS_VALUE")),
Added a default, but low throttle cruise value Added a clear integrator for Rate I to prevent tip ups at launch.
2011-09-23 03:10:55 -03:00
throttle_cruise (THROTTLE_CRUISE, k_param_throttle_cruise, PSTR("TRIM_THROTTLE")),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
allow flight modes to be setup over MAVLink this adopts the same method of setting up flight modes over MAVLink as APM now has git-svn-id: https://arducopter.googlecode.com/svn/trunk@2885 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-17 07:30:53 -03:00
flight_mode1 (FLIGHT_MODE_1, k_param_flight_mode1, PSTR("FLTMODE1")),
flight_mode2 (FLIGHT_MODE_2, k_param_flight_mode2, PSTR("FLTMODE2")),
flight_mode3 (FLIGHT_MODE_3, k_param_flight_mode3, PSTR("FLTMODE3")),
flight_mode4 (FLIGHT_MODE_4, k_param_flight_mode4, PSTR("FLTMODE4")),
flight_mode5 (FLIGHT_MODE_5, k_param_flight_mode5, PSTR("FLTMODE5")),
flight_mode6 (FLIGHT_MODE_6, k_param_flight_mode6, PSTR("FLTMODE6")),
Removed Simple Mode Added Simple option to mode switch positions removed unused OptFlow code added reset lat and lon error removed unused init_auto Fixed log formatting Added simple mode bitmask removed pitchmax added CLI setup for enabling Simple mode to any switch position
2011-09-14 17:58:18 -03:00
simple_modes (0, k_param_simple_modes, PSTR("SIMPLE")),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
re-apply DEFAULT_LOG_BITMASK patch Jason, I assume you removed this patch accidentially git-svn-id: https://arducopter.googlecode.com/svn/trunk@2995 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-08-01 07:06:15 -03:00
log_bitmask (DEFAULT_LOG_BITMASK, k_param_log_bitmask, PSTR("LOG_BITMASK")),
Upped version added new logging params added crosstrack gain re-ordered param inits
2011-11-19 18:00:23 -04:00
log_last_filenumber (0, k_param_log_last_filenumber, PSTR("LOG_LASTFILE")),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
esc_calibrate (0, k_param_esc_calibrate, PSTR("ESC")),
Fixes Alt hold mistake Moves tuning into runtime definable param Added more IMax to throttle Signed-off-by: Jason Short <jasonshort@gmail.com>
2011-09-10 19:16:51 -03:00
radio_tuning (0, k_param_radio_tuning, PSTR("TUNE")),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
frame_orientation (FRAME_ORIENTATION, k_param_frame_orientation, PSTR("FRAME")),
top_bottom_ratio (TOP_BOTTOM_RATIO, k_param_top_bottom_ratio, PSTR("TB_RATIO")),
allow CH7 to be set via params
2011-11-26 17:19:11 -04:00
ch7_option (CH7_SAVE_WP, k_param_ch7_option, PSTR("CH7_OPT")),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
#if FRAME_CONFIG == HELI_FRAME
heli_servo_1 (k_param_heli_servo_1, PSTR("HS1_")),
heli_servo_2 (k_param_heli_servo_2, PSTR("HS2_")),
heli_servo_3 (k_param_heli_servo_3, PSTR("HS3_")),
heli_servo_4 (k_param_heli_servo_4, PSTR("HS4_")),
heli_servo1_pos (-60, k_param_heli_servo1_pos, PSTR("SV1_POS_")),
heli_servo2_pos (60, k_param_heli_servo2_pos, PSTR("SV2_POS_")),
heli_servo3_pos (180, k_param_heli_servo3_pos, PSTR("SV3_POS_")),
heli_roll_max (4500, k_param_heli_roll_max, PSTR("ROL_MAX_")),
heli_pitch_max (4500, k_param_heli_pitch_max, PSTR("PIT_MAX_")),
heli_coll_min (1000, k_param_heli_collective_min, PSTR("COL_MIN_")),
heli_coll_max (2000, k_param_heli_collective_max, PSTR("COL_MAX_")),
heli_coll_mid (1500, k_param_heli_collective_mid, PSTR("COL_MID_")),
heli_ext_gyro_enabled (0, k_param_heli_ext_gyro_enabled, PSTR("GYR_ENABLE_")),
heli_ext_gyro_gain (1000, k_param_heli_ext_gyro_gain, PSTR("GYR_GAIN_")),
TradHeli - added servo averaging to allow support of analog servos - moved heli parameters to 80 because they were causing flight modes to overlap with waypoints
2011-09-25 04:51:25 -03:00
heli_servo_averaging (0, k_param_heli_servo_averaging, PSTR("SV_AVG")),
TradHeli - new parameter HSV_MAN to allow better set-up from APMissionPlanner. Also changed swash movement to use radio_out which fixes some setup bugs
2011-11-12 10:23:07 -04:00
heli_servo_manual (0, k_param_heli_servo_manual, PSTR("HSV_MAN")),
TradHeli - added two parameters to improve heli control. heli_phase_angle allows pilot roll/pitch command to be translated into mixed roll and pitch. heli_coll_yaw_effect mixes some collective into the yaw so tail can counter act collective movements more easily.
2011-11-13 09:20:57 -04:00
heli_phase_angle (0, k_param_heli_phase_angle, PSTR("H_PHANG")),
heli_coll_yaw_effect (0, k_param_heli_coll_yaw_effect, PSTR("H_COLYAW")),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
#endif
// RC channel group key name
//----------------------------------------------------------------------
rc_1 (k_param_rc_1, PSTR("RC1_")),
rc_2 (k_param_rc_2, PSTR("RC2_")),
rc_3 (k_param_rc_3, PSTR("RC3_")),
rc_4 (k_param_rc_4, PSTR("RC4_")),
rc_5 (k_param_rc_5, PSTR("RC5_")),
rc_6 (k_param_rc_6, PSTR("RC6_")),
rc_7 (k_param_rc_7, PSTR("RC7_")),
rc_8 (k_param_rc_8, PSTR("RC8_")),
Added gains to adjust travel of camera.
2011-10-15 20:34:57 -03:00
rc_camera_pitch (k_param_rc_9, PSTR("CAM_P_")),
rc_camera_roll (k_param_rc_10, PSTR("CAM_R_")),
// variable default key name
//-------------------------------------------------------------------------------------------------------------------
typoo in params for camera roll gain. fixed.
2011-10-15 22:34:23 -03:00
camera_pitch_gain (CAM_PITCH_GAIN, k_param_camera_pitch_gain, PSTR("CAM_P_G")),
Added gains to adjust travel of camera.
2011-10-15 20:34:57 -03:00
camera_roll_gain (CAM_ROLL_GAIN, k_param_camera_roll_gain, PSTR("CAM_R_G")),
2.0.35 Added camera reversing parameters in AP_Var Added RTL Throttle Hold set/check Added dynamic speed control to slow down as you reach waypoints and RTL Home upped Yaw Dead zone slightly. git-svn-id: https://arducopter.googlecode.com/svn/trunk@2841 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-12 17:04:15 -03:00
2.0.40 git-svn-id: https://arducopter.googlecode.com/svn/trunk@3252 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-09-04 21:15:36 -03:00
// PI controller group key name initial P initial I initial imax
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
//--------------------------------------------------------------------------------------------------------------------------------------------------------------------
2.0.40 git-svn-id: https://arducopter.googlecode.com/svn/trunk@3252 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-09-04 21:15:36 -03:00
pi_rate_roll (k_param_pi_rate_roll, PSTR("RATE_RLL_"), RATE_ROLL_P, RATE_ROLL_I, RATE_ROLL_IMAX * 100),
pi_rate_pitch (k_param_pi_rate_pitch, PSTR("RATE_PIT_"), RATE_PITCH_P, RATE_PITCH_I, RATE_PITCH_IMAX * 100),
pi_rate_yaw (k_param_pi_rate_yaw, PSTR("RATE_YAW_"), RATE_YAW_P, RATE_YAW_I, RATE_YAW_IMAX * 100),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
2.0.40 git-svn-id: https://arducopter.googlecode.com/svn/trunk@3252 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-09-04 21:15:36 -03:00
pi_stabilize_roll (k_param_pi_stabilize_roll, PSTR("STB_RLL_"), STABILIZE_ROLL_P, STABILIZE_ROLL_I, STABILIZE_ROLL_IMAX * 100),
pi_stabilize_pitch (k_param_pi_stabilize_pitch, PSTR("STB_PIT_"), STABILIZE_PITCH_P, STABILIZE_PITCH_I, STABILIZE_PITCH_IMAX * 100),
pi_stabilize_yaw (k_param_pi_stabilize_yaw, PSTR("STB_YAW_"), STABILIZE_YAW_P, STABILIZE_YAW_I, STABILIZE_YAW_IMAX * 100),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
Shortened loiter PI name to "HLD_LON_" and "HLD_LAT_" git-svn-id: https://arducopter.googlecode.com/svn/trunk@3273 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-09-05 13:00:49 -03:00
pi_loiter_lat (k_param_pi_loiter_lat, PSTR("HLD_LAT_"), LOITER_P, LOITER_I, LOITER_IMAX * 100),
pi_loiter_lon (k_param_pi_loiter_lon, PSTR("HLD_LON_"), LOITER_P, LOITER_I, LOITER_IMAX * 100),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
2.0.40 git-svn-id: https://arducopter.googlecode.com/svn/trunk@3252 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-09-04 21:15:36 -03:00
pi_nav_lat (k_param_pi_nav_lat, PSTR("NAV_LAT_"), NAV_P, NAV_I, NAV_IMAX * 100),
pi_nav_lon (k_param_pi_nav_lon, PSTR("NAV_LON_"), NAV_P, NAV_I, NAV_IMAX * 100),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
Added second PI loop for alt hold. Upped gains for default JDrones Frame added gains for second PI loop for alt removed some tests for 1280 space constraints
2011-10-02 15:36:23 -03:00
pi_alt_hold (k_param_pi_alt_hold, PSTR("THR_ALT_"), THR_HOLD_P, THR_HOLD_I, THR_HOLD_IMAX),
pi_throttle (k_param_pi_throttle, PSTR("THR_RATE_"), THROTTLE_P, THROTTLE_I, THROTTLE_IMAX),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
Added Acro Params Allows user's to fly separate PI loops settings for Acro
2011-10-27 15:52:00 -03:00
pi_acro_roll (k_param_pi_acro_roll, PSTR("ACRO_RLL_"), ACRO_ROLL_P, ACRO_ROLL_I, ACRO_ROLL_IMAX * 100),
pi_acro_pitch (k_param_pi_acro_pitch, PSTR("ACRO_PIT_"), ACRO_PITCH_P, ACRO_PITCH_I, ACRO_PITCH_IMAX * 100),
New PIDs - I rewrote the control laws from scratch to add a PI Rate function. The end result should fly nearly identically to the current version. The nice detail is that we can use NG PID values for easy transition! Before: -> After Stabilize P –> Stabilize P (Use NG values, or 8.3 x the older AC2 value) Stabilize I –> Stabilize I (Stays same value) Stabilize D –> Rate P (Stays same value) –> Rate I (new) Added a new value – an I term for rate. The old stabilization routines did not use this term. Please refer to the config.h file to read more about the new PIDs. Added framework for using DCM corrected Accelerometer rates. Code is commented out for now. Added set home at Arming. Crosstrack is now a full PID loop, rather than just a P gain for more control. Throttle now slews when switching out of Alt hold or Auto modes for less jarring transitions Sonar and Baro PIDs are now combined into a throttle PID Yaw control is completely re-written. Added Octa_Quad support - Max git-svn-id: https://arducopter.googlecode.com/svn/trunk@2836 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-07-10 21:47:08 -03:00
junk(0) // XXX just so that we can add things without worrying about the trailing comma
{
}
updated Param gen - won't compile yet. git-svn-id: https://arducopter.googlecode.com/svn/trunk@1666 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-02-17 03:09:13 -04:00
};
#endif // PARAMETERS_H
2.0.39 Added reset for all nav I when entering manual modes. git-svn-id: https://arducopter.googlecode.com/svn/trunk@2992 f9c3cf11-9bcb-44bc-f272-b75c42450872
2011-08-01 02:12:10 -03:00