mirror of
https://github.com/PX4/PX4-Autopilot.git
synced 2026-05-22 06:14:14 +08:00
fw_att_control: move to px4::params
This commit is contained in:
Daniel Agar
GitHub
Regular → Executable
@@ -20,7 +20,7 @@ px4_add_board(
|
||||
DRIVERS
|
||||
adc
|
||||
barometer/ms5611
|
||||
batt_smbus
|
||||
#batt_smbus
|
||||
camera_capture
|
||||
camera_trigger
|
||||
differential_pressure # all available differential pressure drivers
|
||||
|
||||
File diff suppressed because it is too large
Load Diff
@@ -31,22 +31,23 @@
|
||||
*
|
||||
****************************************************************************/
|
||||
|
||||
#include <px4_module.h>
|
||||
#include <drivers/drv_hrt.h>
|
||||
#include <ecl/attitude_fw/ecl_pitch_controller.h>
|
||||
#include <ecl/attitude_fw/ecl_roll_controller.h>
|
||||
#include <ecl/attitude_fw/ecl_wheel_controller.h>
|
||||
#include <ecl/attitude_fw/ecl_yaw_controller.h>
|
||||
#include <lib/ecl/attitude_fw/ecl_pitch_controller.h>
|
||||
#include <lib/ecl/attitude_fw/ecl_roll_controller.h>
|
||||
#include <lib/ecl/attitude_fw/ecl_wheel_controller.h>
|
||||
#include <lib/ecl/attitude_fw/ecl_yaw_controller.h>
|
||||
#include <lib/ecl/geo/geo.h>
|
||||
#include <mathlib/mathlib.h>
|
||||
#include <lib/mathlib/mathlib.h>
|
||||
#include <lib/parameters/param.h>
|
||||
#include <lib/perf/perf_counter.h>
|
||||
#include <matrix/math.hpp>
|
||||
#include <px4_config.h>
|
||||
#include <px4_defines.h>
|
||||
#include <px4_module.h>
|
||||
#include <px4_module_params.h>
|
||||
#include <px4_platform_common/px4_work_queue/WorkItem.hpp>
|
||||
#include <px4_posix.h>
|
||||
#include <px4_tasks.h>
|
||||
#include <parameters/param.h>
|
||||
#include <perf/perf_counter.h>
|
||||
#include <px4_platform_common/px4_work_queue/WorkItem.hpp>
|
||||
#include <uORB/Publication.hpp>
|
||||
#include <uORB/PublicationMulti.hpp>
|
||||
#include <uORB/Subscription.hpp>
|
||||
@@ -71,7 +72,8 @@ using matrix::Quatf;
|
||||
|
||||
using uORB::SubscriptionData;
|
||||
|
||||
class FixedwingAttitudeControl final : public ModuleBase<FixedwingAttitudeControl>, public px4::WorkItem
|
||||
class FixedwingAttitudeControl final : public ModuleBase<FixedwingAttitudeControl>, public ModuleParams,
|
||||
public px4::WorkItem
|
||||
{
|
||||
public:
|
||||
FixedwingAttitudeControl();
|
||||
@@ -145,147 +147,80 @@ private:
|
||||
|
||||
bool _is_tailsitter{false};
|
||||
|
||||
struct {
|
||||
float p_tc;
|
||||
float p_p;
|
||||
float p_i;
|
||||
float p_ff;
|
||||
float p_rmax_pos;
|
||||
float p_rmax_neg;
|
||||
float p_integrator_max;
|
||||
float r_tc;
|
||||
float r_p;
|
||||
float r_i;
|
||||
float r_ff;
|
||||
float r_integrator_max;
|
||||
float r_rmax;
|
||||
float y_p;
|
||||
float y_i;
|
||||
float y_ff;
|
||||
float y_integrator_max;
|
||||
float roll_to_yaw_ff;
|
||||
float y_rmax;
|
||||
DEFINE_PARAMETERS(
|
||||
(ParamFloat<px4::params::FW_ACRO_X_MAX>) _param_fw_acro_x_max,
|
||||
(ParamFloat<px4::params::FW_ACRO_Y_MAX>) _param_fw_acro_y_max,
|
||||
(ParamFloat<px4::params::FW_ACRO_Z_MAX>) _param_fw_acro_z_max,
|
||||
|
||||
bool w_en;
|
||||
float w_p;
|
||||
float w_i;
|
||||
float w_ff;
|
||||
float w_integrator_max;
|
||||
float w_rmax;
|
||||
(ParamFloat<px4::params::FW_AIRSPD_MAX>) _param_fw_airspd_max,
|
||||
(ParamFloat<px4::params::FW_AIRSPD_MIN>) _param_fw_airspd_min,
|
||||
(ParamFloat<px4::params::FW_AIRSPD_TRIM>) _param_fw_airspd_trim,
|
||||
(ParamInt<px4::params::FW_ARSP_MODE>) _param_fw_arsp_mode,
|
||||
|
||||
float airspeed_min;
|
||||
float airspeed_trim;
|
||||
float airspeed_max;
|
||||
(ParamBool<px4::params::FW_BAT_SCALE_EN>) _param_fw_bat_scale_en,
|
||||
|
||||
float trim_roll;
|
||||
float trim_pitch;
|
||||
float trim_yaw;
|
||||
float dtrim_roll_vmin;
|
||||
float dtrim_pitch_vmin;
|
||||
float dtrim_yaw_vmin;
|
||||
float dtrim_roll_vmax;
|
||||
float dtrim_pitch_vmax;
|
||||
float dtrim_yaw_vmax;
|
||||
float dtrim_roll_flaps;
|
||||
float dtrim_pitch_flaps;
|
||||
float rollsp_offset_deg; /**< Roll Setpoint Offset in deg */
|
||||
float pitchsp_offset_deg; /**< Pitch Setpoint Offset in deg */
|
||||
float rollsp_offset_rad; /**< Roll Setpoint Offset in rad */
|
||||
float pitchsp_offset_rad; /**< Pitch Setpoint Offset in rad */
|
||||
float man_roll_max; /**< Max Roll in rad */
|
||||
float man_pitch_max; /**< Max Pitch in rad */
|
||||
float man_roll_scale; /**< scale factor applied to roll actuator control in pure manual mode */
|
||||
float man_pitch_scale; /**< scale factor applied to pitch actuator control in pure manual mode */
|
||||
float man_yaw_scale; /**< scale factor applied to yaw actuator control in pure manual mode */
|
||||
(ParamFloat<px4::params::FW_DTRIM_P_FLPS>) _param_fw_dtrim_p_flps,
|
||||
(ParamFloat<px4::params::FW_DTRIM_P_VMAX>) _param_fw_dtrim_p_vmax,
|
||||
(ParamFloat<px4::params::FW_DTRIM_P_VMIN>) _param_fw_dtrim_p_vmin,
|
||||
(ParamFloat<px4::params::FW_DTRIM_R_FLPS>) _param_fw_dtrim_r_flps,
|
||||
(ParamFloat<px4::params::FW_DTRIM_R_VMAX>) _param_fw_dtrim_r_vmax,
|
||||
(ParamFloat<px4::params::FW_DTRIM_R_VMIN>) _param_fw_dtrim_r_vmin,
|
||||
(ParamFloat<px4::params::FW_DTRIM_Y_VMAX>) _param_fw_dtrim_y_vmax,
|
||||
(ParamFloat<px4::params::FW_DTRIM_Y_VMIN>) _param_fw_dtrim_y_vmin,
|
||||
|
||||
float acro_max_x_rate_rad;
|
||||
float acro_max_y_rate_rad;
|
||||
float acro_max_z_rate_rad;
|
||||
(ParamFloat<px4::params::FW_FLAPERON_SCL>) _param_fw_flaperon_scl,
|
||||
(ParamFloat<px4::params::FW_FLAPS_LND_SCL>) _param_fw_flaps_lnd_scl,
|
||||
(ParamFloat<px4::params::FW_FLAPS_SCL>) _param_fw_flaps_scl,
|
||||
(ParamFloat<px4::params::FW_FLAPS_TO_SCL>) _param_fw_flaps_to_scl,
|
||||
|
||||
float flaps_scale; /**< Scale factor for flaps */
|
||||
float flaps_takeoff_scale; /**< Scale factor for flaps on take-off */
|
||||
float flaps_land_scale; /**< Scale factor for flaps on landing */
|
||||
float flaperon_scale; /**< Scale factor for flaperons */
|
||||
(ParamFloat<px4::params::FW_MAN_P_MAX>) _param_fw_man_p_max,
|
||||
(ParamFloat<px4::params::FW_MAN_P_SC>) _param_fw_man_p_sc,
|
||||
(ParamFloat<px4::params::FW_MAN_R_MAX>) _param_fw_man_r_max,
|
||||
(ParamFloat<px4::params::FW_MAN_R_SC>) _param_fw_man_r_sc,
|
||||
(ParamFloat<px4::params::FW_MAN_Y_SC>) _param_fw_man_y_sc,
|
||||
|
||||
float rattitude_thres;
|
||||
(ParamFloat<px4::params::FW_P_RMAX_NEG>) _param_fw_p_rmax_neg,
|
||||
(ParamFloat<px4::params::FW_P_RMAX_POS>) _param_fw_p_rmax_pos,
|
||||
(ParamFloat<px4::params::FW_P_TC>) _param_fw_p_tc,
|
||||
(ParamFloat<px4::params::FW_PR_FF>) _param_fw_pr_ff,
|
||||
(ParamFloat<px4::params::FW_PR_I>) _param_fw_pr_i,
|
||||
(ParamFloat<px4::params::FW_PR_IMAX>) _param_fw_pr_imax,
|
||||
(ParamFloat<px4::params::FW_PR_P>) _param_fw_pr_p,
|
||||
(ParamFloat<px4::params::FW_PSP_OFF>) _param_fw_psp_off,
|
||||
|
||||
int32_t bat_scale_en; /**< Battery scaling enabled */
|
||||
bool airspeed_disabled;
|
||||
(ParamFloat<px4::params::FW_RATT_TH>) _param_fw_ratt_th,
|
||||
|
||||
} _parameters{}; /**< local copies of interesting parameters */
|
||||
(ParamFloat<px4::params::FW_R_RMAX>) _param_fw_r_rmax,
|
||||
(ParamFloat<px4::params::FW_R_TC>) _param_fw_r_tc,
|
||||
(ParamFloat<px4::params::FW_RLL_TO_YAW_FF>) _param_fw_rll_to_yaw_ff,
|
||||
(ParamFloat<px4::params::FW_RR_FF>) _param_fw_rr_ff,
|
||||
(ParamFloat<px4::params::FW_RR_I>) _param_fw_rr_i,
|
||||
(ParamFloat<px4::params::FW_RR_IMAX>) _param_fw_rr_imax,
|
||||
(ParamFloat<px4::params::FW_RR_P>) _param_fw_rr_p,
|
||||
(ParamFloat<px4::params::FW_RSP_OFF>) _param_fw_rsp_off,
|
||||
|
||||
struct {
|
||||
(ParamBool<px4::params::FW_W_EN>) _param_fw_w_en,
|
||||
(ParamFloat<px4::params::FW_W_RMAX>) _param_fw_w_rmax,
|
||||
(ParamFloat<px4::params::FW_WR_FF>) _param_fw_wr_ff,
|
||||
(ParamFloat<px4::params::FW_WR_I>) _param_fw_wr_i,
|
||||
(ParamFloat<px4::params::FW_WR_IMAX>) _param_fw_wr_imax,
|
||||
(ParamFloat<px4::params::FW_WR_P>) _param_fw_wr_p,
|
||||
|
||||
param_t p_tc;
|
||||
param_t p_p;
|
||||
param_t p_i;
|
||||
param_t p_ff;
|
||||
param_t p_rmax_pos;
|
||||
param_t p_rmax_neg;
|
||||
param_t p_integrator_max;
|
||||
param_t r_tc;
|
||||
param_t r_p;
|
||||
param_t r_i;
|
||||
param_t r_ff;
|
||||
param_t r_integrator_max;
|
||||
param_t r_rmax;
|
||||
param_t y_p;
|
||||
param_t y_i;
|
||||
param_t y_ff;
|
||||
param_t y_integrator_max;
|
||||
param_t roll_to_yaw_ff;
|
||||
param_t y_rmax;
|
||||
(ParamFloat<px4::params::FW_Y_RMAX>) _param_fw_y_rmax,
|
||||
(ParamFloat<px4::params::FW_YR_FF>) _param_fw_yr_ff,
|
||||
(ParamFloat<px4::params::FW_YR_I>) _param_fw_yr_i,
|
||||
(ParamFloat<px4::params::FW_YR_IMAX>) _param_fw_yr_imax,
|
||||
(ParamFloat<px4::params::FW_YR_P>) _param_fw_yr_p,
|
||||
|
||||
param_t w_en;
|
||||
param_t w_p;
|
||||
param_t w_i;
|
||||
param_t w_ff;
|
||||
param_t w_integrator_max;
|
||||
param_t w_rmax;
|
||||
(ParamFloat<px4::params::TRIM_PITCH>) _param_trim_pitch,
|
||||
(ParamFloat<px4::params::TRIM_ROLL>) _param_trim_roll,
|
||||
(ParamFloat<px4::params::TRIM_YAW>) _param_trim_yaw
|
||||
)
|
||||
|
||||
param_t airspeed_min;
|
||||
param_t airspeed_trim;
|
||||
param_t airspeed_max;
|
||||
|
||||
param_t trim_roll;
|
||||
param_t trim_pitch;
|
||||
param_t trim_yaw;
|
||||
param_t dtrim_roll_vmin;
|
||||
param_t dtrim_pitch_vmin;
|
||||
param_t dtrim_yaw_vmin;
|
||||
param_t dtrim_roll_vmax;
|
||||
param_t dtrim_pitch_vmax;
|
||||
param_t dtrim_yaw_vmax;
|
||||
param_t dtrim_roll_flaps;
|
||||
param_t dtrim_pitch_flaps;
|
||||
param_t rollsp_offset_deg;
|
||||
param_t pitchsp_offset_deg;
|
||||
param_t man_roll_max;
|
||||
param_t man_pitch_max;
|
||||
param_t man_roll_scale;
|
||||
param_t man_pitch_scale;
|
||||
param_t man_yaw_scale;
|
||||
|
||||
param_t acro_max_x_rate;
|
||||
param_t acro_max_y_rate;
|
||||
param_t acro_max_z_rate;
|
||||
|
||||
param_t flaps_scale;
|
||||
param_t flaps_takeoff_scale;
|
||||
param_t flaps_land_scale;
|
||||
param_t flaperon_scale;
|
||||
|
||||
param_t rattitude_thres;
|
||||
|
||||
param_t bat_scale_en;
|
||||
param_t airspeed_mode;
|
||||
|
||||
} _parameter_handles{}; /**< handles for interesting parameters */
|
||||
|
||||
ECL_RollController _roll_ctrl;
|
||||
ECL_PitchController _pitch_ctrl;
|
||||
ECL_YawController _yaw_ctrl;
|
||||
ECL_WheelController _wheel_ctrl;
|
||||
ECL_RollController _roll_ctrl;
|
||||
ECL_PitchController _pitch_ctrl;
|
||||
ECL_YawController _yaw_ctrl;
|
||||
ECL_WheelController _wheel_ctrl;
|
||||
|
||||
void control_flaps(const float dt);
|
||||
|
||||
|
||||
Reference in New Issue
Block a user