ardupilot/Blimp/Loiter.cpp

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#include "Blimp.h"
#include <AC_AttitudeControl/AC_PosControl.h>
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#define MA 0.99
#define MO (1-MA)
void Loiter::run(Vector3f& target_pos, float& target_yaw, Vector4b axes_disabled)
{
const float dt = blimp.scheduler.get_last_loop_time_s();
float scaler_xz_n;
float xz_out = fabsf(blimp.motors->front_out) + fabsf(blimp.motors->down_out);
if (xz_out > 1) {
scaler_xz_n = 1 / xz_out;
} else {
scaler_xz_n = 1;
}
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scaler_xz = scaler_xz*MA + scaler_xz_n*MO;
float scaler_yyaw_n;
float yyaw_out = fabsf(blimp.motors->right_out) + fabsf(blimp.motors->yaw_out);
if (yyaw_out > 1) {
scaler_yyaw_n = 1 / yyaw_out;
} else {
scaler_yyaw_n = 1;
}
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scaler_yyaw = scaler_yyaw*MA + scaler_yyaw_n*MO;
#if HAL_LOGGING_ENABLED
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AP::logger().WriteStreaming("BSC", "TimeUS,xz,yyaw,xzn,yyawn",
"Qffff",
AP_HAL::micros64(),
scaler_xz, scaler_yyaw, scaler_xz_n, scaler_yyaw_n);
#endif
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float yaw_ef = blimp.ahrs.get_yaw();
Vector3f err_xyz = target_pos - blimp.pos_ned;
float err_yaw = wrap_PI(target_yaw - yaw_ef);
Vector4b zero;
if ((fabsf(err_xyz.x) < blimp.g.pid_dz) || !blimp.motors->_armed || (blimp.g.dis_mask & (1<<(2-1)))) {
zero.x = true;
}
if ((fabsf(err_xyz.y) < blimp.g.pid_dz) || !blimp.motors->_armed || (blimp.g.dis_mask & (1<<(1-1)))) {
zero.y = true;
}
if ((fabsf(err_xyz.z) < blimp.g.pid_dz) || !blimp.motors->_armed || (blimp.g.dis_mask & (1<<(3-1)))) {
zero.z = true;
}
if ((fabsf(err_yaw) < blimp.g.pid_dz) || !blimp.motors->_armed || (blimp.g.dis_mask & (1<<(4-1)))) {
zero.yaw = true;
}
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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."
Vector4b limit = zero || axes_disabled;
Vector3f target_vel_ef;
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};
if (!axes_disabled.z) {
target_vel_ef.z = blimp.pid_pos_z.update_all(target_pos.z, blimp.pos_ned.z, dt, limit.z);
}
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float target_vel_yaw = 0;
if (!axes_disabled.yaw) {
target_vel_yaw = blimp.pid_pos_yaw.update_error(wrap_PI(target_yaw - yaw_ef), dt, limit.yaw);
blimp.pid_pos_yaw.set_target_rate(target_yaw);
blimp.pid_pos_yaw.set_actual_rate(yaw_ef);
}
Vector3f target_vel_ef_c{constrain_float(target_vel_ef.x, -blimp.g.max_vel_xy, blimp.g.max_vel_xy),
constrain_float(target_vel_ef.y, -blimp.g.max_vel_xy, blimp.g.max_vel_xy),
constrain_float(target_vel_ef.z, -blimp.g.max_vel_z, blimp.g.max_vel_z)};
float target_vel_yaw_c = constrain_float(target_vel_yaw, -blimp.g.max_vel_yaw, blimp.g.max_vel_yaw);
Vector2f target_vel_ef_c_scaled_xy = {target_vel_ef_c.x * scaler_xz, target_vel_ef_c.y * scaler_yyaw};
Vector2f vel_ned_filtd_scaled_xy = {blimp.vel_ned_filtd.x * scaler_xz, blimp.vel_ned_filtd.y * scaler_yyaw};
Vector2f actuator;
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});
float act_down = 0;
if (!axes_disabled.z) {
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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blimp.rotate_NE_to_BF(actuator);
float act_yaw = 0;
if (!axes_disabled.yaw) {
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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if (!blimp.motors->armed()) {
blimp.pid_pos_xy.set_integrator(Vector2f(0,0));
blimp.pid_pos_z.set_integrator(0);
blimp.pid_pos_yaw.set_integrator(0);
blimp.pid_vel_xy.set_integrator(Vector2f(0,0));
blimp.pid_vel_z.set_integrator(0);
blimp.pid_vel_yaw.set_integrator(0);
target_pos = blimp.pos_ned;
target_yaw = blimp.ahrs.get_yaw();
}
if (zero.x) {
blimp.motors->front_out = 0;
} else if (axes_disabled.x);
else {
blimp.motors->front_out = actuator.x;
}
if (zero.y) {
blimp.motors->right_out = 0;
} else if (axes_disabled.y);
else {
blimp.motors->right_out = actuator.y;
}
if (zero.z) {
blimp.motors->down_out = 0;
} else if (axes_disabled.z);
else {
blimp.motors->down_out = act_down;
}
if (zero.yaw) {
blimp.motors->yaw_out = 0;
} else if (axes_disabled.yaw);
else {
blimp.motors->yaw_out = act_yaw;
}
#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);
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);
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);
#endif
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}
void Loiter::run_vel(Vector3f& target_vel_ef, float& target_vel_yaw, Vector4b axes_disabled)
{
const float dt = blimp.scheduler.get_last_loop_time_s();
Vector4b zero;
if (!blimp.motors->_armed || (blimp.g.dis_mask & (1<<(2-1)))) {
zero.x = true;
}
if (!blimp.motors->_armed || (blimp.g.dis_mask & (1<<(1-1)))) {
zero.y = true;
}
if (!blimp.motors->_armed || (blimp.g.dis_mask & (1<<(3-1)))) {
zero.z = true;
}
if (!blimp.motors->_armed || (blimp.g.dis_mask & (1<<(4-1)))) {
zero.yaw = true;
}
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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."
Vector4b limit = zero || axes_disabled;
Vector3f target_vel_ef_c{constrain_float(target_vel_ef.x, -blimp.g.max_vel_xy, blimp.g.max_vel_xy),
constrain_float(target_vel_ef.y, -blimp.g.max_vel_xy, blimp.g.max_vel_xy),
constrain_float(target_vel_ef.z, -blimp.g.max_vel_z, blimp.g.max_vel_z)};
float target_vel_yaw_c = constrain_float(target_vel_yaw, -blimp.g.max_vel_yaw, blimp.g.max_vel_yaw);
Vector2f target_vel_ef_c_scaled_xy = {target_vel_ef_c.x * scaler_xz, target_vel_ef_c.y * scaler_yyaw};
Vector2f vel_ned_filtd_scaled_xy = {blimp.vel_ned_filtd.x * scaler_xz, blimp.vel_ned_filtd.y * scaler_yyaw};
Vector2f actuator;
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});
float act_down = 0;
if (!axes_disabled.z) {
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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blimp.rotate_NE_to_BF(actuator);
float act_yaw = 0;
if (!axes_disabled.yaw) {
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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if (!blimp.motors->armed()) {
blimp.pid_vel_xy.set_integrator(Vector2f(0,0));
blimp.pid_vel_z.set_integrator(0);
blimp.pid_vel_yaw.set_integrator(0);
}
if (zero.x) {
blimp.motors->front_out = 0;
} else if (axes_disabled.x);
else {
blimp.motors->front_out = actuator.x;
}
if (zero.y) {
blimp.motors->right_out = 0;
} else if (axes_disabled.y);
else {
blimp.motors->right_out = actuator.y;
}
if (zero.z) {
blimp.motors->down_out = 0;
} else if (axes_disabled.z);
else {
blimp.motors->down_out = act_down;
}
if (zero.yaw) {
blimp.motors->yaw_out = 0;
} else if (axes_disabled.yaw);
else {
blimp.motors->yaw_out = act_yaw;
}
#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);
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);
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);
#endif
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}