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author | Thomas Gubler <thomasgubler@gmail.com> | 2014-12-02 12:19:24 +0100 |
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committer | Thomas Gubler <thomasgubler@gmail.com> | 2014-12-02 12:19:24 +0100 |
commit | e28e8c11bba0779386fc16ee47deac4db39b51c0 (patch) | |
tree | e86866463bd88c5d1c11bbd0db14152a26e0e05c /src/modules | |
parent | 141dda209222a7dd5afad6b844735fd9a44756a6 (diff) | |
download | px4-firmware-e28e8c11bba0779386fc16ee47deac4db39b51c0.tar.gz px4-firmware-e28e8c11bba0779386fc16ee47deac4db39b51c0.tar.bz2 px4-firmware-e28e8c11bba0779386fc16ee47deac4db39b51c0.zip |
make default apps compatible with autogenerated attitude and rc_channels message
Diffstat (limited to 'src/modules')
7 files changed, 69 insertions, 64 deletions
diff --git a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp index e2dbc30dd..8d537d676 100755 --- a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp +++ b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp @@ -549,7 +549,7 @@ const unsigned int loop_interval_alarm = 6500; // loop interval in microseconds R = R_decl * R_body; /* copy rotation matrix */ - memcpy(&att.R[0][0], &R.data[0][0], sizeof(att.R)); + memcpy(&att.R[0], &R.data[0][0], sizeof(att.R)); att.R_valid = true; if (isfinite(att.roll) && isfinite(att.pitch) && isfinite(att.yaw)) { diff --git a/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp index e7805daa9..db6773b8a 100644 --- a/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp +++ b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp @@ -83,6 +83,7 @@ #include <systemlib/systemlib.h> #include <mathlib/mathlib.h> #include <mavlink/mavlink_log.h> +#include <px4_defines.h> #include "estimator_23states.h" @@ -1384,7 +1385,7 @@ FixedwingEstimator::task_main() math::Vector<3> euler = R.to_euler(); for (int i = 0; i < 3; i++) for (int j = 0; j < 3; j++) - _att.R[i][j] = R(i, j); + PX4_R(_att.R, i, j) = R(i, j); _att.timestamp = _last_sensor_timestamp; _att.q[0] = _ekf->states[0]; diff --git a/src/modules/fw_att_control/fw_att_control_main.cpp b/src/modules/fw_att_control/fw_att_control_main.cpp index e770c11a2..83fe25571 100644 --- a/src/modules/fw_att_control/fw_att_control_main.cpp +++ b/src/modules/fw_att_control/fw_att_control_main.cpp @@ -75,6 +75,7 @@ #include <ecl/attitude_fw/ecl_pitch_controller.h> #include <ecl/attitude_fw/ecl_roll_controller.h> #include <ecl/attitude_fw/ecl_yaw_controller.h> +#include <px4_defines.h> /** * Fixedwing attitude control app start / stop handling function @@ -824,9 +825,9 @@ FixedwingAttitudeControl::task_main() float speed_body_v = 0.0f; float speed_body_w = 0.0f; if(_att.R_valid) { - speed_body_u = _att.R[0][0] * _global_pos.vel_n + _att.R[1][0] * _global_pos.vel_e + _att.R[2][0] * _global_pos.vel_d; - speed_body_v = _att.R[0][1] * _global_pos.vel_n + _att.R[1][1] * _global_pos.vel_e + _att.R[2][1] * _global_pos.vel_d; - speed_body_w = _att.R[0][2] * _global_pos.vel_n + _att.R[1][2] * _global_pos.vel_e + _att.R[2][2] * _global_pos.vel_d; + speed_body_u = PX4_R(_att.R, 0, 0) * _global_pos.vel_n + PX4_R(_att.R, 1, 0) * _global_pos.vel_e + PX4_R(_att.R, 2, 0) * _global_pos.vel_d; + speed_body_v = PX4_R(_att.R, 0, 1) * _global_pos.vel_n + PX4_R(_att.R, 1, 1) * _global_pos.vel_e + PX4_R(_att.R, 2, 1) * _global_pos.vel_d; + speed_body_w = PX4_R(_att.R, 0, 2) * _global_pos.vel_n + PX4_R(_att.R, 1, 2) * _global_pos.vel_e + PX4_R(_att.R, 2, 2) * _global_pos.vel_d; } else { if (_debug && loop_counter % 10 == 0) { warnx("Did not get a valid R\n"); diff --git a/src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp b/src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp index 6017369aa..f441c4a91 100644 --- a/src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp +++ b/src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp @@ -90,6 +90,7 @@ #include <external_lgpl/tecs/tecs.h> #include "landingslope.h" #include "mtecs/mTecs.h" +#include <px4_defines.h> static int _control_task = -1; /**< task handle for sensor task */ @@ -704,7 +705,7 @@ FixedwingPositionControl::vehicle_attitude_poll() /* set rotation matrix */ for (int i = 0; i < 3; i++) for (int j = 0; j < 3; j++) - _R_nb(i, j) = _att.R[i][j]; + _R_nb(i, j) = PX4_R(_att.R, i, j); } } diff --git a/src/modules/mc_pos_control/mc_pos_control_main.cpp b/src/modules/mc_pos_control/mc_pos_control_main.cpp index 5918d6bc5..6682a9c89 100644 --- a/src/modules/mc_pos_control/mc_pos_control_main.cpp +++ b/src/modules/mc_pos_control/mc_pos_control_main.cpp @@ -73,6 +73,7 @@ #include <mathlib/mathlib.h> #include <lib/geo/geo.h> #include <mavlink/mavlink_log.h> +#include <px4_defines.h> #define TILT_COS_MAX 0.7f #define SIGMA 0.000001f @@ -1147,11 +1148,11 @@ MulticopterPositionControl::task_main() /* thrust compensation for altitude only control mode */ float att_comp; - if (_att.R[2][2] > TILT_COS_MAX) { - att_comp = 1.0f / _att.R[2][2]; + if (PX4_R(_att.R, 2, 2) > TILT_COS_MAX) { + att_comp = 1.0f / PX4_R(_att.R, 2, 2); - } else if (_att.R[2][2] > 0.0f) { - att_comp = ((1.0f / TILT_COS_MAX - 1.0f) / TILT_COS_MAX) * _att.R[2][2] + 1.0f; + } else if (PX4_R(_att.R, 2, 2) > 0.0f) { + att_comp = ((1.0f / TILT_COS_MAX - 1.0f) / TILT_COS_MAX) * PX4_R(_att.R, 2, 2) + 1.0f; saturation_z = true; } else { diff --git a/src/modules/position_estimator_inav/position_estimator_inav_main.c b/src/modules/position_estimator_inav/position_estimator_inav_main.c index 296919c04..2a601b630 100644 --- a/src/modules/position_estimator_inav/position_estimator_inav_main.c +++ b/src/modules/position_estimator_inav/position_estimator_inav_main.c @@ -68,6 +68,7 @@ #include <geo/geo.h> #include <systemlib/systemlib.h> #include <drivers/drv_hrt.h> +#include <px4_defines.h> #include "position_estimator_inav_params.h" #include "inertial_filter.h" @@ -282,13 +283,13 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) }; float w_gps_xy = 1.0f; float w_gps_z = 1.0f; - + float corr_vision[3][2] = { { 0.0f, 0.0f }, // N (pos, vel) { 0.0f, 0.0f }, // E (pos, vel) { 0.0f, 0.0f }, // D (pos, vel) }; - + float corr_sonar = 0.0f; float corr_sonar_filtered = 0.0f; @@ -461,7 +462,7 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) acc[i] = 0.0f; for (int j = 0; j < 3; j++) { - acc[i] += att.R[i][j] * sensor.accelerometer_m_s2[j]; + acc[i] += PX4_R(att.R, i, j) * sensor.accelerometer_m_s2[j]; } } @@ -494,7 +495,7 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) if ((flow.ground_distance_m > 0.31f) && (flow.ground_distance_m < 4.0f) && - (att.R[2][2] > 0.7f) && + (PX4_R(att.R, 2, 2) > 0.7f) && (fabsf(flow.ground_distance_m - sonar_prev) > FLT_EPSILON)) { sonar_time = t; @@ -531,15 +532,15 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) float flow_q = flow.quality / 255.0f; float dist_bottom = - z_est[0] - surface_offset; - if (dist_bottom > 0.3f && flow_q > params.flow_q_min && (t < sonar_valid_time + sonar_valid_timeout) && att.R[2][2] > 0.7f) { + if (dist_bottom > 0.3f && flow_q > params.flow_q_min && (t < sonar_valid_time + sonar_valid_timeout) && PX4_R(att.R, 2, 2) > 0.7f) { /* distance to surface */ - float flow_dist = dist_bottom / att.R[2][2]; + float flow_dist = dist_bottom / PX4_R(att.R, 2, 2); /* check if flow if too large for accurate measurements */ /* calculate estimated velocity in body frame */ float body_v_est[2] = { 0.0f, 0.0f }; for (int i = 0; i < 2; i++) { - body_v_est[i] = att.R[0][i] * x_est[1] + att.R[1][i] * y_est[1] + att.R[2][i] * z_est[1]; + body_v_est[i] = PX4_R(att.R, 0, i) * x_est[1] + PX4_R(att.R, 1, i) * y_est[1] + PX4_R(att.R, 2, i) * z_est[1]; } /* set this flag if flow should be accurate according to current velocity and attitude rate estimate */ @@ -562,7 +563,7 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) /* project measurements vector to NED basis, skip Z component */ for (int i = 0; i < 2; i++) { for (int j = 0; j < 3; j++) { - flow_v[i] += att.R[i][j] * flow_m[j]; + flow_v[i] += PX4_R(att.R, i, j) * flow_m[j]; } } @@ -571,7 +572,7 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) corr_flow[1] = flow_v[1] - y_est[1]; /* adjust correction weight */ float flow_q_weight = (flow_q - params.flow_q_min) / (1.0f - params.flow_q_min); - w_flow = att.R[2][2] * flow_q_weight / fmaxf(1.0f, flow_dist); + w_flow = PX4_R(att.R, 2, 2) * flow_q_weight / fmaxf(1.0f, flow_dist); /* if flow is not accurate, reduce weight for it */ // TODO make this more fuzzy @@ -646,13 +647,13 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) x_est[1] = vision.vx; y_est[0] = vision.y; y_est[1] = vision.vy; - /* only reset the z estimate if the z weight parameter is not zero */ + /* only reset the z estimate if the z weight parameter is not zero */ if (params.w_z_vision_p > MIN_VALID_W) { z_est[0] = vision.z; z_est[1] = vision.vz; } - + vision_valid = true; warnx("VISION estimate valid"); mavlink_log_info(mavlink_fd, "[inav] VISION estimate valid"); @@ -912,7 +913,7 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) float c = 0.0f; for (int j = 0; j < 3; j++) { - c += att.R[j][i] * accel_bias_corr[j]; + c += PX4_R(att.R, j, i) * accel_bias_corr[j]; } if (isfinite(c)) { @@ -937,7 +938,7 @@ int position_estimator_inav_thread_main(int argc, char *argv[]) float c = 0.0f; for (int j = 0; j < 3; j++) { - c += att.R[j][i] * accel_bias_corr[j]; + c += PX4_R(att.R, j, i) * accel_bias_corr[j]; } if (isfinite(c)) { diff --git a/src/modules/sensors/sensors.cpp b/src/modules/sensors/sensors.cpp index cdcb428dd..672dc52c3 100644 --- a/src/modules/sensors/sensors.cpp +++ b/src/modules/sensors/sensors.cpp @@ -182,13 +182,13 @@ private: /** * Get and limit value for specified RC function. Returns NAN if not mapped. */ - float get_rc_value(enum RC_CHANNELS_FUNCTION func, float min_value, float max_value); + float get_rc_value(uint8_t func, float min_value, float max_value); /** * Get switch position for specified function. */ - switch_pos_t get_rc_sw3pos_position(enum RC_CHANNELS_FUNCTION func, float on_th, bool on_inv, float mid_th, bool mid_inv); - switch_pos_t get_rc_sw2pos_position(enum RC_CHANNELS_FUNCTION func, float on_th, bool on_inv); + switch_pos_t get_rc_sw3pos_position(uint8_t func, float on_th, bool on_inv, float mid_th, bool mid_inv); + switch_pos_t get_rc_sw2pos_position(uint8_t func, float on_th, bool on_inv); /** * Gather and publish RC input data. @@ -771,25 +771,25 @@ Sensors::parameters_update() _parameters.rc_offboard_th = fabs(_parameters.rc_offboard_th); /* update RC function mappings */ - _rc.function[THROTTLE] = _parameters.rc_map_throttle - 1; - _rc.function[ROLL] = _parameters.rc_map_roll - 1; - _rc.function[PITCH] = _parameters.rc_map_pitch - 1; - _rc.function[YAW] = _parameters.rc_map_yaw - 1; - - _rc.function[MODE] = _parameters.rc_map_mode_sw - 1; - _rc.function[RETURN] = _parameters.rc_map_return_sw - 1; - _rc.function[POSCTL] = _parameters.rc_map_posctl_sw - 1; - _rc.function[LOITER] = _parameters.rc_map_loiter_sw - 1; - _rc.function[ACRO] = _parameters.rc_map_acro_sw - 1; - _rc.function[OFFBOARD] = _parameters.rc_map_offboard_sw - 1; - - _rc.function[FLAPS] = _parameters.rc_map_flaps - 1; - - _rc.function[AUX_1] = _parameters.rc_map_aux1 - 1; - _rc.function[AUX_2] = _parameters.rc_map_aux2 - 1; - _rc.function[AUX_3] = _parameters.rc_map_aux3 - 1; - _rc.function[AUX_4] = _parameters.rc_map_aux4 - 1; - _rc.function[AUX_5] = _parameters.rc_map_aux5 - 1; + _rc.function[RC_CHANNELS_FUNCTION_THROTTLE] = _parameters.rc_map_throttle - 1; + _rc.function[RC_CHANNELS_FUNCTION_ROLL] = _parameters.rc_map_roll - 1; + _rc.function[RC_CHANNELS_FUNCTION_PITCH] = _parameters.rc_map_pitch - 1; + _rc.function[RC_CHANNELS_FUNCTION_YAW] = _parameters.rc_map_yaw - 1; + + _rc.function[RC_CHANNELS_FUNCTION_MODE] = _parameters.rc_map_mode_sw - 1; + _rc.function[RC_CHANNELS_FUNCTION_RETURN] = _parameters.rc_map_return_sw - 1; + _rc.function[RC_CHANNELS_FUNCTION_POSCTL] = _parameters.rc_map_posctl_sw - 1; + _rc.function[RC_CHANNELS_FUNCTION_LOITER] = _parameters.rc_map_loiter_sw - 1; + _rc.function[RC_CHANNELS_FUNCTION_ACRO] = _parameters.rc_map_acro_sw - 1; + _rc.function[RC_CHANNELS_FUNCTION_OFFBOARD] = _parameters.rc_map_offboard_sw - 1; + + _rc.function[RC_CHANNELS_FUNCTION_FLAPS] = _parameters.rc_map_flaps - 1; + + _rc.function[RC_CHANNELS_FUNCTION_AUX_1] = _parameters.rc_map_aux1 - 1; + _rc.function[RC_CHANNELS_FUNCTION_AUX_2] = _parameters.rc_map_aux2 - 1; + _rc.function[RC_CHANNELS_FUNCTION_AUX_3] = _parameters.rc_map_aux3 - 1; + _rc.function[RC_CHANNELS_FUNCTION_AUX_4] = _parameters.rc_map_aux4 - 1; + _rc.function[RC_CHANNELS_FUNCTION_AUX_5] = _parameters.rc_map_aux5 - 1; /* gyro offsets */ param_get(_parameter_handles.gyro_offset[0], &(_parameters.gyro_offset[0])); @@ -1492,7 +1492,7 @@ Sensors::adc_poll(struct sensor_combined_s &raw) } float -Sensors::get_rc_value(enum RC_CHANNELS_FUNCTION func, float min_value, float max_value) +Sensors::get_rc_value(uint8_t func, float min_value, float max_value) { if (_rc.function[func] >= 0) { float value = _rc.channels[_rc.function[func]]; @@ -1513,7 +1513,7 @@ Sensors::get_rc_value(enum RC_CHANNELS_FUNCTION func, float min_value, float max } switch_pos_t -Sensors::get_rc_sw3pos_position(enum RC_CHANNELS_FUNCTION func, float on_th, bool on_inv, float mid_th, bool mid_inv) +Sensors::get_rc_sw3pos_position(uint8_t func, float on_th, bool on_inv, float mid_th, bool mid_inv) { if (_rc.function[func] >= 0) { float value = 0.5f * _rc.channels[_rc.function[func]] + 0.5f; @@ -1534,7 +1534,7 @@ Sensors::get_rc_sw3pos_position(enum RC_CHANNELS_FUNCTION func, float on_th, boo } switch_pos_t -Sensors::get_rc_sw2pos_position(enum RC_CHANNELS_FUNCTION func, float on_th, bool on_inv) +Sensors::get_rc_sw2pos_position(uint8_t func, float on_th, bool on_inv) { if (_rc.function[func] >= 0) { float value = 0.5f * _rc.channels[_rc.function[func]] + 0.5f; @@ -1668,24 +1668,24 @@ Sensors::rc_poll() manual.timestamp = rc_input.timestamp_last_signal; /* limit controls */ - manual.y = get_rc_value(ROLL, -1.0, 1.0); - manual.x = get_rc_value(PITCH, -1.0, 1.0); - manual.r = get_rc_value(YAW, -1.0, 1.0); - manual.z = get_rc_value(THROTTLE, 0.0, 1.0); - manual.flaps = get_rc_value(FLAPS, -1.0, 1.0); - manual.aux1 = get_rc_value(AUX_1, -1.0, 1.0); - manual.aux2 = get_rc_value(AUX_2, -1.0, 1.0); - manual.aux3 = get_rc_value(AUX_3, -1.0, 1.0); - manual.aux4 = get_rc_value(AUX_4, -1.0, 1.0); - manual.aux5 = get_rc_value(AUX_5, -1.0, 1.0); + manual.y = get_rc_value(RC_CHANNELS_FUNCTION_ROLL, -1.0, 1.0); + manual.x = get_rc_value(RC_CHANNELS_FUNCTION_PITCH, -1.0, 1.0); + manual.r = get_rc_value(RC_CHANNELS_FUNCTION_YAW, -1.0, 1.0); + manual.z = get_rc_value(RC_CHANNELS_FUNCTION_THROTTLE, 0.0, 1.0); + manual.flaps = get_rc_value(RC_CHANNELS_FUNCTION_FLAPS, -1.0, 1.0); + manual.aux1 = get_rc_value(RC_CHANNELS_FUNCTION_AUX_1, -1.0, 1.0); + manual.aux2 = get_rc_value(RC_CHANNELS_FUNCTION_AUX_2, -1.0, 1.0); + manual.aux3 = get_rc_value(RC_CHANNELS_FUNCTION_AUX_3, -1.0, 1.0); + manual.aux4 = get_rc_value(RC_CHANNELS_FUNCTION_AUX_4, -1.0, 1.0); + manual.aux5 = get_rc_value(RC_CHANNELS_FUNCTION_AUX_5, -1.0, 1.0); /* mode switches */ - manual.mode_switch = get_rc_sw3pos_position(MODE, _parameters.rc_auto_th, _parameters.rc_auto_inv, _parameters.rc_assist_th, _parameters.rc_assist_inv); - manual.posctl_switch = get_rc_sw2pos_position(POSCTL, _parameters.rc_posctl_th, _parameters.rc_posctl_inv); - manual.return_switch = get_rc_sw2pos_position(RETURN, _parameters.rc_return_th, _parameters.rc_return_inv); - manual.loiter_switch = get_rc_sw2pos_position(LOITER, _parameters.rc_loiter_th, _parameters.rc_loiter_inv); - manual.acro_switch = get_rc_sw2pos_position(ACRO, _parameters.rc_acro_th, _parameters.rc_acro_inv); - manual.offboard_switch = get_rc_sw2pos_position(OFFBOARD, _parameters.rc_offboard_th, _parameters.rc_offboard_inv); + manual.mode_switch = get_rc_sw3pos_position(RC_CHANNELS_FUNCTION_MODE, _parameters.rc_auto_th, _parameters.rc_auto_inv, _parameters.rc_assist_th, _parameters.rc_assist_inv); + manual.posctl_switch = get_rc_sw2pos_position(RC_CHANNELS_FUNCTION_POSCTL, _parameters.rc_posctl_th, _parameters.rc_posctl_inv); + manual.return_switch = get_rc_sw2pos_position(RC_CHANNELS_FUNCTION_RETURN, _parameters.rc_return_th, _parameters.rc_return_inv); + manual.loiter_switch = get_rc_sw2pos_position(RC_CHANNELS_FUNCTION_LOITER, _parameters.rc_loiter_th, _parameters.rc_loiter_inv); + manual.acro_switch = get_rc_sw2pos_position(RC_CHANNELS_FUNCTION_ACRO, _parameters.rc_acro_th, _parameters.rc_acro_inv); + manual.offboard_switch = get_rc_sw2pos_position(RC_CHANNELS_FUNCTION_OFFBOARD, _parameters.rc_offboard_th, _parameters.rc_offboard_inv); /* publish manual_control_setpoint topic */ if (_manual_control_pub > 0) { |