mirror of https://github.com/ArduPilot/ardupilot
211 lines
8.4 KiB
C++
211 lines
8.4 KiB
C++
#include "Blimp.h"
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#include <AC_AttitudeControl/AC_PosControl.h>
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#define MA 0.99
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#define MO (1-MA)
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void Loiter::run(Vector3f& target_pos, float& target_yaw, Vector4b axes_disabled)
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{
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const float dt = blimp.scheduler.get_last_loop_time_s();
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float scaler_xz_n;
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float xz_out = fabsf(blimp.motors->front_out) + fabsf(blimp.motors->down_out);
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if (xz_out > 1) {
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scaler_xz_n = 1 / xz_out;
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} else {
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scaler_xz_n = 1;
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}
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scaler_xz = scaler_xz*MA + scaler_xz_n*MO;
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float scaler_yyaw_n;
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float yyaw_out = fabsf(blimp.motors->right_out) + fabsf(blimp.motors->yaw_out);
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if (yyaw_out > 1) {
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scaler_yyaw_n = 1 / yyaw_out;
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} else {
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scaler_yyaw_n = 1;
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}
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scaler_yyaw = scaler_yyaw*MA + scaler_yyaw_n*MO;
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#if HAL_LOGGING_ENABLED
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AP::logger().WriteStreaming("BSC", "TimeUS,xz,yyaw,xzn,yyawn",
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"Qffff",
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AP_HAL::micros64(),
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scaler_xz, scaler_yyaw, scaler_xz_n, scaler_yyaw_n);
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#endif
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float yaw_ef = blimp.ahrs.get_yaw();
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Vector3f err_xyz = target_pos - blimp.pos_ned;
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float err_yaw = wrap_PI(target_yaw - yaw_ef);
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Vector4b zero;
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if ((fabsf(err_xyz.x) < blimp.g.pid_dz) || !blimp.motors->_armed || (blimp.g.dis_mask & (1<<(2-1)))) {
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zero.x = true;
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}
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if ((fabsf(err_xyz.y) < blimp.g.pid_dz) || !blimp.motors->_armed || (blimp.g.dis_mask & (1<<(1-1)))) {
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zero.y = true;
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}
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if ((fabsf(err_xyz.z) < blimp.g.pid_dz) || !blimp.motors->_armed || (blimp.g.dis_mask & (1<<(3-1)))) {
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zero.z = true;
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}
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if ((fabsf(err_yaw) < blimp.g.pid_dz) || !blimp.motors->_armed || (blimp.g.dis_mask & (1<<(4-1)))) {
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zero.yaw = true;
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}
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//Disabled means "don't update PIDs or output anything at all". Zero means actually output zero thrust. I term is limited in either case."
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Vector4b limit = zero || axes_disabled;
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Vector3f target_vel_ef;
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if (!axes_disabled.x && !axes_disabled.y) target_vel_ef = {blimp.pid_pos_xy.update_all(target_pos, blimp.pos_ned, dt, {(float)limit.x, (float)limit.y, (float)limit.z}), 0};
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if (!axes_disabled.z) {
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target_vel_ef.z = blimp.pid_pos_z.update_all(target_pos.z, blimp.pos_ned.z, dt, limit.z);
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}
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float target_vel_yaw = 0;
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if (!axes_disabled.yaw) {
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target_vel_yaw = blimp.pid_pos_yaw.update_error(wrap_PI(target_yaw - yaw_ef), dt, limit.yaw);
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blimp.pid_pos_yaw.set_target_rate(target_yaw);
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blimp.pid_pos_yaw.set_actual_rate(yaw_ef);
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}
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Vector3f target_vel_ef_c{constrain_float(target_vel_ef.x, -blimp.g.max_vel_xy, blimp.g.max_vel_xy),
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constrain_float(target_vel_ef.y, -blimp.g.max_vel_xy, blimp.g.max_vel_xy),
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constrain_float(target_vel_ef.z, -blimp.g.max_vel_z, blimp.g.max_vel_z)};
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float target_vel_yaw_c = constrain_float(target_vel_yaw, -blimp.g.max_vel_yaw, blimp.g.max_vel_yaw);
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Vector2f target_vel_ef_c_scaled_xy = {target_vel_ef_c.x * scaler_xz, target_vel_ef_c.y * scaler_yyaw};
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Vector2f vel_ned_filtd_scaled_xy = {blimp.vel_ned_filtd.x * scaler_xz, blimp.vel_ned_filtd.y * scaler_yyaw};
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Vector2f actuator;
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if (!axes_disabled.x && !axes_disabled.y) actuator = blimp.pid_vel_xy.update_all(target_vel_ef_c_scaled_xy, vel_ned_filtd_scaled_xy, dt, {(float)limit.x, (float)limit.y});
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float act_down = 0;
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if (!axes_disabled.z) {
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act_down = blimp.pid_vel_z.update_all(target_vel_ef_c.z * scaler_xz, blimp.vel_ned_filtd.z * scaler_xz, dt, limit.z);
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}
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blimp.rotate_NE_to_BF(actuator);
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float act_yaw = 0;
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if (!axes_disabled.yaw) {
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act_yaw = blimp.pid_vel_yaw.update_all(target_vel_yaw_c * scaler_yyaw, blimp.vel_yaw_filtd * scaler_yyaw, dt, limit.yaw);
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}
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if (!blimp.motors->armed()) {
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blimp.pid_pos_xy.set_integrator(Vector2f(0,0));
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blimp.pid_pos_z.set_integrator(0);
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blimp.pid_pos_yaw.set_integrator(0);
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blimp.pid_vel_xy.set_integrator(Vector2f(0,0));
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blimp.pid_vel_z.set_integrator(0);
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blimp.pid_vel_yaw.set_integrator(0);
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target_pos = blimp.pos_ned;
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target_yaw = blimp.ahrs.get_yaw();
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}
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if (zero.x) {
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blimp.motors->front_out = 0;
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} else if (axes_disabled.x);
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else {
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blimp.motors->front_out = actuator.x;
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}
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if (zero.y) {
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blimp.motors->right_out = 0;
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} else if (axes_disabled.y);
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else {
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blimp.motors->right_out = actuator.y;
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}
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if (zero.z) {
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blimp.motors->down_out = 0;
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} else if (axes_disabled.z);
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else {
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blimp.motors->down_out = act_down;
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}
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if (zero.yaw) {
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blimp.motors->yaw_out = 0;
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} else if (axes_disabled.yaw);
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else {
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blimp.motors->yaw_out = act_yaw;
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}
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#if HAL_LOGGING_ENABLED
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AC_PosControl::Write_PSCN(0.0, target_pos.x * 100.0, blimp.pos_ned.x * 100.0, 0.0, target_vel_ef_c.x * 100.0, blimp.vel_ned_filtd.x * 100.0, 0.0, 0.0, 0.0);
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AC_PosControl::Write_PSCE(0.0, target_pos.y * 100.0, blimp.pos_ned.y * 100.0, 0.0, target_vel_ef_c.y * 100.0, blimp.vel_ned_filtd.y * 100.0, 0.0, 0.0, 0.0);
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AC_PosControl::Write_PSCD(0.0, -target_pos.z * 100.0, -blimp.pos_ned.z * 100.0, 0.0, -target_vel_ef_c.z * 100.0, -blimp.vel_ned_filtd.z * 100.0, 0.0, 0.0, 0.0);
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#endif
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}
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void Loiter::run_vel(Vector3f& target_vel_ef, float& target_vel_yaw, Vector4b axes_disabled)
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{
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const float dt = blimp.scheduler.get_last_loop_time_s();
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Vector4b zero;
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if (!blimp.motors->_armed || (blimp.g.dis_mask & (1<<(2-1)))) {
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zero.x = true;
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}
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if (!blimp.motors->_armed || (blimp.g.dis_mask & (1<<(1-1)))) {
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zero.y = true;
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}
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if (!blimp.motors->_armed || (blimp.g.dis_mask & (1<<(3-1)))) {
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zero.z = true;
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}
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if (!blimp.motors->_armed || (blimp.g.dis_mask & (1<<(4-1)))) {
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zero.yaw = true;
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}
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//Disabled means "don't update PIDs or output anything at all". Zero means actually output zero thrust. I term is limited in either case."
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Vector4b limit = zero || axes_disabled;
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Vector3f target_vel_ef_c{constrain_float(target_vel_ef.x, -blimp.g.max_vel_xy, blimp.g.max_vel_xy),
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constrain_float(target_vel_ef.y, -blimp.g.max_vel_xy, blimp.g.max_vel_xy),
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constrain_float(target_vel_ef.z, -blimp.g.max_vel_z, blimp.g.max_vel_z)};
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float target_vel_yaw_c = constrain_float(target_vel_yaw, -blimp.g.max_vel_yaw, blimp.g.max_vel_yaw);
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Vector2f target_vel_ef_c_scaled_xy = {target_vel_ef_c.x * scaler_xz, target_vel_ef_c.y * scaler_yyaw};
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Vector2f vel_ned_filtd_scaled_xy = {blimp.vel_ned_filtd.x * scaler_xz, blimp.vel_ned_filtd.y * scaler_yyaw};
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Vector2f actuator;
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if (!axes_disabled.x && !axes_disabled.y) actuator = blimp.pid_vel_xy.update_all(target_vel_ef_c_scaled_xy, vel_ned_filtd_scaled_xy, dt, {(float)limit.x, (float)limit.y});
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float act_down = 0;
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if (!axes_disabled.z) {
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act_down = blimp.pid_vel_z.update_all(target_vel_ef_c.z * scaler_xz, blimp.vel_ned_filtd.z * scaler_xz, dt, limit.z);
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}
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blimp.rotate_NE_to_BF(actuator);
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float act_yaw = 0;
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if (!axes_disabled.yaw) {
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act_yaw = blimp.pid_vel_yaw.update_all(target_vel_yaw_c * scaler_yyaw, blimp.vel_yaw_filtd * scaler_yyaw, dt, limit.yaw);
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}
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if (!blimp.motors->armed()) {
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blimp.pid_vel_xy.set_integrator(Vector2f(0,0));
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blimp.pid_vel_z.set_integrator(0);
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blimp.pid_vel_yaw.set_integrator(0);
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}
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if (zero.x) {
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blimp.motors->front_out = 0;
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} else if (axes_disabled.x);
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else {
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blimp.motors->front_out = actuator.x;
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}
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if (zero.y) {
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blimp.motors->right_out = 0;
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} else if (axes_disabled.y);
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else {
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blimp.motors->right_out = actuator.y;
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}
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if (zero.z) {
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blimp.motors->down_out = 0;
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} else if (axes_disabled.z);
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else {
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blimp.motors->down_out = act_down;
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}
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if (zero.yaw) {
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blimp.motors->yaw_out = 0;
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} else if (axes_disabled.yaw);
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else {
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blimp.motors->yaw_out = act_yaw;
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}
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#if HAL_LOGGING_ENABLED
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AC_PosControl::Write_PSCN(0.0, 0.0, blimp.pos_ned.x * 100.0, 0.0, target_vel_ef_c.x * 100.0, blimp.vel_ned_filtd.x * 100.0, 0.0, 0.0, 0.0);
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AC_PosControl::Write_PSCE(0.0, 0.0, blimp.pos_ned.y * 100.0, 0.0, target_vel_ef_c.y * 100.0, blimp.vel_ned_filtd.y * 100.0, 0.0, 0.0, 0.0);
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AC_PosControl::Write_PSCD(0.0, 0.0, -blimp.pos_ned.z * 100.0, 0.0, -target_vel_ef_c.z * 100.0, -blimp.vel_ned_filtd.z * 100.0, 0.0, 0.0, 0.0);
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#endif
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}
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