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Merge branch 'master' of github.com:PX4/Firmware

sbg
Lorenz Meier 12 years ago
parent
commit
238f018090
  1. 16
      ROMFS/px4fmu_common/init.d/10_dji_f330
  2. 1
      src/modules/commander/commander_params.c
  3. 13
      src/modules/multirotor_pos_control/multirotor_pos_control.c
  4. 4
      src/modules/multirotor_pos_control/multirotor_pos_control_params.c
  5. 4
      src/modules/multirotor_pos_control/multirotor_pos_control_params.h
  6. 4
      src/modules/px4iofirmware/mixer.cpp

16
ROMFS/px4fmu_common/init.d/10_dji_f330

@ -22,6 +22,22 @@ then
param set MC_YAWRATE_D 0.005 param set MC_YAWRATE_D 0.005
param set MC_YAWRATE_I 0.2 param set MC_YAWRATE_I 0.2
param set MC_YAWRATE_P 0.3 param set MC_YAWRATE_P 0.3
param set NAV_TAKEOFF_ALT 1.0
param set MPC_TILT_MAX 0.5
param set MPC_THR_MAX 0.7
param set MPC_THR_MIN 0.3
param set MPC_XY_D 0
param set MPC_XY_P 0.5
param set MPC_XY_VEL_D 0
param set MPC_XY_VEL_I 0
param set MPC_XY_VEL_MAX 2
param set MPC_XY_VEL_P 0.2
param set MPC_Z_D 0
param set MPC_Z_P 1
param set MPC_Z_VEL_D 0
param set MPC_Z_VEL_I 0.10
param set MPC_Z_VEL_MAX 2
param set MPC_Z_VEL_P 0.20
param save param save
fi fi

1
src/modules/commander/commander_params.c

@ -46,6 +46,7 @@
#include <systemlib/param/param.h> #include <systemlib/param/param.h>
PARAM_DEFINE_FLOAT(NAV_TAKEOFF_ALT, 5.0f); PARAM_DEFINE_FLOAT(NAV_TAKEOFF_ALT, 5.0f);
PARAM_DEFINE_FLOAT(NAV_TAKEOFF_GAP, 3.0f);
PARAM_DEFINE_FLOAT(TRIM_ROLL, 0.0f); PARAM_DEFINE_FLOAT(TRIM_ROLL, 0.0f);
PARAM_DEFINE_FLOAT(TRIM_PITCH, 0.0f); PARAM_DEFINE_FLOAT(TRIM_PITCH, 0.0f);
PARAM_DEFINE_FLOAT(TRIM_YAW, 0.0f); PARAM_DEFINE_FLOAT(TRIM_YAW, 0.0f);

13
src/modules/multirotor_pos_control/multirotor_pos_control.c

@ -227,7 +227,7 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
hrt_abstime t_prev = 0; hrt_abstime t_prev = 0;
const float alt_ctl_dz = 0.2f; const float alt_ctl_dz = 0.2f;
const float pos_ctl_dz = 0.05f; const float pos_ctl_dz = 0.05f;
const float takeoff_alt_default = 10.0f;
float ref_alt = 0.0f; float ref_alt = 0.0f;
hrt_abstime ref_alt_t = 0; hrt_abstime ref_alt_t = 0;
uint64_t local_ref_timestamp = 0; uint64_t local_ref_timestamp = 0;
@ -244,6 +244,7 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
parameters_init(&params_h); parameters_init(&params_h);
parameters_update(&params_h, &params); parameters_update(&params_h, &params);
for (int i = 0; i < 2; i++) { for (int i = 0; i < 2; i++) {
pid_init(&(xy_pos_pids[i]), params.xy_p, 0.0f, params.xy_d, 1.0f, 0.0f, PID_MODE_DERIVATIV_SET, 0.02f); pid_init(&(xy_pos_pids[i]), params.xy_p, 0.0f, params.xy_d, 1.0f, 0.0f, PID_MODE_DERIVATIV_SET, 0.02f);
pid_init(&(xy_vel_pids[i]), params.xy_vel_p, params.xy_vel_i, params.xy_vel_d, 1.0f, params.tilt_max, PID_MODE_DERIVATIV_CALC_NO_SP, 0.02f); pid_init(&(xy_vel_pids[i]), params.xy_vel_p, params.xy_vel_i, params.xy_vel_d, 1.0f, params.tilt_max, PID_MODE_DERIVATIV_CALC_NO_SP, 0.02f);
@ -350,7 +351,7 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
if (reset_sp_z) { if (reset_sp_z) {
reset_sp_z = false; reset_sp_z = false;
local_pos_sp.z = local_pos.z; local_pos_sp.z = local_pos.z;
mavlink_log_info(mavlink_fd, "[mpc] reset alt sp: %.2f", (double)-local_pos_sp.z); mavlink_log_info(mavlink_fd, "[mpc] reset alt sp: %.2f", (double) - local_pos_sp.z);
} }
/* move altitude setpoint with throttle stick */ /* move altitude setpoint with throttle stick */
@ -423,12 +424,12 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
if (reset_auto_pos) { if (reset_auto_pos) {
local_pos_sp.x = local_pos.x; local_pos_sp.x = local_pos.x;
local_pos_sp.y = local_pos.y; local_pos_sp.y = local_pos.y;
local_pos_sp.z = -takeoff_alt_default; local_pos_sp.z = - params.takeoff_alt - params.takeoff_gap;
local_pos_sp.yaw = att.yaw; local_pos_sp.yaw = att.yaw;
local_pos_sp_valid = true; local_pos_sp_valid = true;
att_sp.yaw_body = att.yaw; att_sp.yaw_body = att.yaw;
reset_auto_pos = false; reset_auto_pos = false;
mavlink_log_info(mavlink_fd, "[mpc] takeoff sp: %.2f %.2f %.2f", (double)local_pos_sp.x, (double)local_pos_sp.y, (double)-local_pos_sp.z); mavlink_log_info(mavlink_fd, "[mpc] takeoff sp: %.2f %.2f %.2f", (double)local_pos_sp.x, (double)local_pos_sp.y, (double) - local_pos_sp.z);
} }
} else if (control_mode.auto_state == NAVIGATION_STATE_AUTO_RTL) { } else if (control_mode.auto_state == NAVIGATION_STATE_AUTO_RTL) {
@ -504,7 +505,7 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
/* set altitude setpoint to 5m under ground, /* set altitude setpoint to 5m under ground,
* don't set it too deep to avoid unexpected landing in case of false "landed" signal */ * don't set it too deep to avoid unexpected landing in case of false "landed" signal */
local_pos_sp.z = 5.0f; local_pos_sp.z = 5.0f;
mavlink_log_info(mavlink_fd, "[mpc] landed, set alt: %.2f", (double)-local_pos_sp.z); mavlink_log_info(mavlink_fd, "[mpc] landed, set alt: %.2f", (double) - local_pos_sp.z);
} }
reset_sp_z = true; reset_sp_z = true;
@ -514,7 +515,7 @@ static int multirotor_pos_control_thread_main(int argc, char *argv[])
if (reset_sp_z) { if (reset_sp_z) {
reset_sp_z = false; reset_sp_z = false;
local_pos_sp.z = local_pos.z; local_pos_sp.z = local_pos.z;
mavlink_log_info(mavlink_fd, "[mpc] set loiter alt: %.2f", (double)-local_pos_sp.z); mavlink_log_info(mavlink_fd, "[mpc] set loiter alt: %.2f", (double) - local_pos_sp.z);
} }
} }

4
src/modules/multirotor_pos_control/multirotor_pos_control_params.c

@ -59,6 +59,8 @@ PARAM_DEFINE_FLOAT(MPC_TILT_MAX, 0.5f);
int parameters_init(struct multirotor_position_control_param_handles *h) int parameters_init(struct multirotor_position_control_param_handles *h)
{ {
h->takeoff_alt = param_find("NAV_TAKEOFF_ALT");
h->takeoff_gap = param_find("NAV_TAKEOFF_GAP");
h->thr_min = param_find("MPC_THR_MIN"); h->thr_min = param_find("MPC_THR_MIN");
h->thr_max = param_find("MPC_THR_MAX"); h->thr_max = param_find("MPC_THR_MAX");
h->z_p = param_find("MPC_Z_P"); h->z_p = param_find("MPC_Z_P");
@ -84,6 +86,8 @@ int parameters_init(struct multirotor_position_control_param_handles *h)
int parameters_update(const struct multirotor_position_control_param_handles *h, struct multirotor_position_control_params *p) int parameters_update(const struct multirotor_position_control_param_handles *h, struct multirotor_position_control_params *p)
{ {
param_get(h->takeoff_alt, &(p->takeoff_alt));
param_get(h->takeoff_gap, &(p->takeoff_gap));
param_get(h->thr_min, &(p->thr_min)); param_get(h->thr_min, &(p->thr_min));
param_get(h->thr_max, &(p->thr_max)); param_get(h->thr_max, &(p->thr_max));
param_get(h->z_p, &(p->z_p)); param_get(h->z_p, &(p->z_p));

4
src/modules/multirotor_pos_control/multirotor_pos_control_params.h

@ -41,6 +41,8 @@
#include <systemlib/param/param.h> #include <systemlib/param/param.h>
struct multirotor_position_control_params { struct multirotor_position_control_params {
float takeoff_alt;
float takeoff_gap;
float thr_min; float thr_min;
float thr_max; float thr_max;
float z_p; float z_p;
@ -63,6 +65,8 @@ struct multirotor_position_control_params {
}; };
struct multirotor_position_control_param_handles { struct multirotor_position_control_param_handles {
param_t takeoff_alt;
param_t takeoff_gap;
param_t thr_min; param_t thr_min;
param_t thr_max; param_t thr_max;
param_t z_p; param_t z_p;

4
src/modules/px4iofirmware/mixer.cpp

@ -358,8 +358,8 @@ static unsigned mixer_text_length = 0;
void void
mixer_handle_text(const void *buffer, size_t length) mixer_handle_text(const void *buffer, size_t length)
{ {
/* do not allow a mixer change while outputs armed */ /* do not allow a mixer change while safety off */
if ((r_status_flags & PX4IO_P_STATUS_FLAGS_OUTPUTS_ARMED)) { if ((r_status_flags & PX4IO_P_STATUS_FLAGS_SAFETY_OFF)) {
return; return;
} }

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