mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-06 13:48:52 +08:00
Merge remote-tracking branch 'px4/master' into navigator_rewrite
Conflicts: src/modules/position_estimator_inav/position_estimator_inav_main.c
This commit is contained in:
+12
-2
@@ -69,6 +69,9 @@ UBX::UBX(const int &fd, struct vehicle_gps_position_s *gps_position) :
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_gps_position(gps_position),
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_configured(false),
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_waiting_for_ack(false),
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_got_posllh(false),
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_got_velned(false),
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_got_timeutc(false),
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_disable_cmd_last(0)
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{
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decode_init();
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@@ -275,9 +278,10 @@ UBX::receive(unsigned timeout)
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bool handled = false;
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while (true) {
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bool ready_to_return = _configured ? (_got_posllh && _got_velned && _got_timeutc) : handled;
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/* poll for new data, wait for only UBX_PACKET_TIMEOUT (2ms) if something already received */
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int ret = poll(fds, sizeof(fds) / sizeof(fds[0]), handled ? UBX_PACKET_TIMEOUT : timeout);
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int ret = poll(fds, sizeof(fds) / sizeof(fds[0]), ready_to_return ? UBX_PACKET_TIMEOUT : timeout);
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if (ret < 0) {
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/* something went wrong when polling */
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@@ -286,7 +290,10 @@ UBX::receive(unsigned timeout)
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} else if (ret == 0) {
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/* return success after short delay after receiving a packet or timeout after long delay */
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if (handled) {
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if (ready_to_return) {
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_got_posllh = false;
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_got_velned = false;
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_got_timeutc = false;
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return 1;
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} else {
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@@ -438,6 +445,7 @@ UBX::handle_message()
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_rate_count_lat_lon++;
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_got_posllh = true;
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ret = 1;
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break;
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}
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@@ -482,6 +490,7 @@ UBX::handle_message()
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_gps_position->time_gps_usec += (uint64_t)(packet->time_nanoseconds * 1e-3f);
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_gps_position->timestamp_time = hrt_absolute_time();
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_got_timeutc = true;
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ret = 1;
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break;
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}
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@@ -557,6 +566,7 @@ UBX::handle_message()
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_rate_count_vel++;
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_got_velned = true;
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ret = 1;
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break;
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}
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@@ -397,6 +397,9 @@ private:
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struct vehicle_gps_position_s *_gps_position;
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bool _configured;
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bool _waiting_for_ack;
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bool _got_posllh;
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bool _got_velned;
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bool _got_timeutc;
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uint8_t _message_class_needed;
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uint8_t _message_id_needed;
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ubx_decode_state_t _decode_state;
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@@ -61,9 +61,9 @@ ECL_PitchController::ECL_PitchController() :
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_integrator(0.0f),
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_rate_error(0.0f),
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_rate_setpoint(0.0f),
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_bodyrate_setpoint(0.0f)
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_bodyrate_setpoint(0.0f),
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_nonfinite_input_perf(perf_alloc(PC_COUNT, "fw att control pitch nonfinite input"))
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{
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perf_alloc(PC_COUNT, "fw att control pitch nonfinite input");
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}
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ECL_PitchController::~ECL_PitchController()
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@@ -59,9 +59,9 @@ ECL_RollController::ECL_RollController() :
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_integrator(0.0f),
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_rate_error(0.0f),
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_rate_setpoint(0.0f),
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_bodyrate_setpoint(0.0f)
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_bodyrate_setpoint(0.0f),
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_nonfinite_input_perf(perf_alloc(PC_COUNT, "fw att control roll nonfinite input"))
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{
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perf_alloc(PC_COUNT, "fw att control roll nonfinite input");
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}
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ECL_RollController::~ECL_RollController()
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@@ -58,9 +58,9 @@ ECL_YawController::ECL_YawController() :
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_rate_error(0.0f),
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_rate_setpoint(0.0f),
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_bodyrate_setpoint(0.0f),
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_coordinated_min_speed(1.0f)
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_coordinated_min_speed(1.0f),
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_nonfinite_input_perf(perf_alloc(PC_COUNT, "fw att control yaw nonfinite input"))
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{
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perf_alloc(PC_COUNT, "fw att control yaw nonfinite input");
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}
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ECL_YawController::~ECL_YawController()
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@@ -71,19 +71,20 @@
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#include "inertial_filter.h"
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#define MIN_VALID_W 0.00001f
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#define PUB_INTERVAL 10000 // limit publish rate to 100 Hz
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#define EST_BUF_SIZE 250000 / PUB_INTERVAL // buffer size is 0.5s
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static bool thread_should_exit = false; /**< Deamon exit flag */
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static bool thread_running = false; /**< Deamon status flag */
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static int position_estimator_inav_task; /**< Handle of deamon task / thread */
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static bool verbose_mode = false;
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static const hrt_abstime gps_topic_timeout = 1000000; // GPS topic timeout = 1s
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static const hrt_abstime gps_topic_timeout = 500000; // GPS topic timeout = 0.5s
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static const hrt_abstime flow_topic_timeout = 1000000; // optical flow topic timeout = 1s
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static const hrt_abstime sonar_timeout = 150000; // sonar timeout = 150ms
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static const hrt_abstime sonar_valid_timeout = 1000000; // estimate sonar distance during this time after sonar loss
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static const hrt_abstime xy_src_timeout = 2000000; // estimate position during this time after position sources loss
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static const uint32_t updates_counter_len = 1000000;
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static const uint32_t pub_interval = 10000; // limit publish rate to 100 Hz
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static const float max_flow = 1.0f; // max flow value that can be used, rad/s
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__EXPORT int position_estimator_inav_main(int argc, char *argv[]);
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@@ -92,6 +93,16 @@ int position_estimator_inav_thread_main(int argc, char *argv[]);
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static void usage(const char *reason);
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static inline int min(int val1, int val2)
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{
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return (val1 < val2) ? val1 : val2;
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}
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static inline int max(int val1, int val2)
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{
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return (val1 > val2) ? val1 : val2;
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}
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/**
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* Print the correct usage.
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*/
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@@ -135,7 +146,7 @@ int position_estimator_inav_main(int argc, char *argv[])
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thread_should_exit = false;
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position_estimator_inav_task = task_spawn_cmd("position_estimator_inav",
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SCHED_DEFAULT, SCHED_PRIORITY_MAX - 5, 4000,
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SCHED_DEFAULT, SCHED_PRIORITY_MAX - 5, 5000,
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position_estimator_inav_thread_main,
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(argv) ? (const char **) &argv[2] : (const char **) NULL);
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exit(0);
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@@ -199,8 +210,21 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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float y_est[2] = { 0.0f, 0.0f }; // pos, vel
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float z_est[2] = { 0.0f, 0.0f }; // pos, vel
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float eph = 1.0;
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float epv = 1.0;
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float est_buf[EST_BUF_SIZE][3][2]; // estimated position buffer
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float R_buf[EST_BUF_SIZE][3][3]; // rotation matrix buffer
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float R_gps[3][3]; // rotation matrix for GPS correction moment
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memset(est_buf, 0, sizeof(est_buf));
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memset(R_buf, 0, sizeof(R_buf));
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memset(R_gps, 0, sizeof(R_gps));
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int buf_ptr = 0;
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static const float min_eph_epv = 2.0f; // min EPH/EPV, used for weight calculation
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static const float max_eph_epv = 20.0f; // max EPH/EPV acceptable for estimation
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float eph = max_eph_epv;
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float epv = 1.0f;
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float eph_flow = 1.0f;
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float x_est_prev[2], y_est_prev[2], z_est_prev[2];
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memset(x_est_prev, 0, sizeof(x_est_prev));
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@@ -257,9 +281,6 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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float corr_flow[] = { 0.0f, 0.0f }; // N E
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float w_flow = 0.0f;
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static float min_eph_epv = 2.0f; // min EPH/EPV, used for weight calculation
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static float max_eph_epv = 10.0f; // max EPH/EPV acceptable for estimation
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float sonar_prev = 0.0f;
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hrt_abstime flow_prev = 0; // time of last flow measurement
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hrt_abstime sonar_time = 0; // time of last sonar measurement (not filtered)
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@@ -536,9 +557,10 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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w_flow *= 0.05f;
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}
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flow_valid = true;
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/* under ideal conditions, on 1m distance assume EPH = 10cm */
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eph_flow = 0.1 / w_flow;
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eph = fminf(eph, 0.1 / att.R[2][2] / flow_q * fmaxf(1.0f, flow_dist)); // under ideal conditions, on 1m distance assume EPH = 10cm
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flow_valid = true;
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} else {
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w_flow = 0.0f;
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@@ -597,13 +619,13 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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/* hysteresis for GPS quality */
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if (gps_valid) {
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if (gps.eph > max_eph_epv * 1.5f || gps.epv > max_eph_epv * 1.5f || gps.fix_type < 3) {
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if (gps.eph > max_eph_epv || gps.epv > max_eph_epv || gps.fix_type < 3) {
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gps_valid = false;
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mavlink_log_info(mavlink_fd, "[inav] GPS signal lost");
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}
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} else {
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if (gps.eph < max_eph_epv && gps.epv < max_eph_epv && gps.fix_type >= 3) {
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if (gps.eph < max_eph_epv * 0.7f && gps.epv < max_eph_epv * 0.7f && gps.fix_type >= 3) {
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gps_valid = true;
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reset_est = true;
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mavlink_log_info(mavlink_fd, "[inav] GPS signal found");
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@@ -657,16 +679,22 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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y_est[1] = gps.vel_e_m_s;
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}
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/* calculate index of estimated values in buffer */
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int est_i = buf_ptr - 1 - min(EST_BUF_SIZE - 1, max(0, (int)(params.delay_gps * 1000000.0f / PUB_INTERVAL)));
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if (est_i < 0) {
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est_i += EST_BUF_SIZE;
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}
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/* calculate correction for position */
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corr_gps[0][0] = gps_proj[0] - x_est[0];
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corr_gps[1][0] = gps_proj[1] - y_est[0];
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corr_gps[2][0] = local_pos.ref_alt - alt - z_est[0];
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corr_gps[0][0] = gps_proj[0] - est_buf[est_i][0][0];
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corr_gps[1][0] = gps_proj[1] - est_buf[est_i][1][0];
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corr_gps[2][0] = local_pos.ref_alt - alt - est_buf[est_i][2][0];
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/* calculate correction for velocity */
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if (gps.vel_ned_valid) {
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corr_gps[0][1] = gps.vel_n_m_s - x_est[1];
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corr_gps[1][1] = gps.vel_e_m_s - y_est[1];
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corr_gps[2][1] = gps.vel_d_m_s - z_est[1];
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corr_gps[0][1] = gps.vel_n_m_s - est_buf[est_i][0][1];
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corr_gps[1][1] = gps.vel_e_m_s - est_buf[est_i][1][1];
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corr_gps[2][1] = gps.vel_d_m_s - est_buf[est_i][2][1];
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} else {
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corr_gps[0][1] = 0.0f;
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@@ -674,8 +702,8 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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corr_gps[2][1] = 0.0f;
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}
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eph = fminf(eph, gps.eph);
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epv = fminf(epv, gps.epv);
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/* save rotation matrix at this moment */
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memcpy(R_gps, R_buf[est_i], sizeof(R_gps));
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w_gps_xy = min_eph_epv / fmaxf(min_eph_epv, gps.eph);
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w_gps_z = min_eph_epv / fmaxf(min_eph_epv, gps.epv);
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@@ -717,8 +745,12 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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t_prev = t;
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/* increase EPH/EPV on each step */
|
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eph *= 1.0 + dt;
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epv += 0.005 * dt; // add 1m to EPV each 200s (baro drift)
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if (eph < max_eph_epv) {
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eph *= 1.0 + dt;
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}
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if (epv < max_eph_epv) {
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epv += 0.005 * dt; // add 1m to EPV each 200s (baro drift)
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}
|
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|
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/* use GPS if it's valid and reference position initialized */
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bool use_gps_xy = ref_inited && gps_valid && params.w_xy_gps_p > MIN_VALID_W;
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@@ -731,7 +763,7 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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xy_src_time = t;
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}
|
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|
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bool can_estimate_xy = eph < max_eph_epv * 1.5;
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bool can_estimate_xy = (eph < max_eph_epv) || use_gps_xy || use_flow;
|
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|
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bool dist_bottom_valid = (t < sonar_valid_time + sonar_valid_timeout);
|
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|
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@@ -763,7 +795,7 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
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corr_baro += offs_corr;
|
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}
|
||||
|
||||
/* accelerometer bias correction */
|
||||
/* accelerometer bias correction for GPS (use buffered rotation matrix) */
|
||||
float accel_bias_corr[3] = { 0.0f, 0.0f, 0.0f };
|
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|
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if (use_gps_xy) {
|
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@@ -777,6 +809,24 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
|
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accel_bias_corr[2] -= corr_gps[2][0] * w_z_gps_p * w_z_gps_p;
|
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}
|
||||
|
||||
/* transform error vector from NED frame to body frame */
|
||||
for (int i = 0; i < 3; i++) {
|
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float c = 0.0f;
|
||||
|
||||
for (int j = 0; j < 3; j++) {
|
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c += R_gps[j][i] * accel_bias_corr[j];
|
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}
|
||||
|
||||
if (isfinite(c)) {
|
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acc_bias[i] += c * params.w_acc_bias * dt;
|
||||
}
|
||||
}
|
||||
|
||||
/* accelerometer bias correction for flow and baro (assume that there is no delay) */
|
||||
accel_bias_corr[0] = 0.0f;
|
||||
accel_bias_corr[1] = 0.0f;
|
||||
accel_bias_corr[2] = 0.0f;
|
||||
|
||||
if (use_flow) {
|
||||
accel_bias_corr[0] -= corr_flow[0] * params.w_xy_flow;
|
||||
accel_bias_corr[1] -= corr_flow[1] * params.w_xy_flow;
|
||||
@@ -807,7 +857,12 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
|
||||
|
||||
/* inertial filter correction for altitude */
|
||||
inertial_filter_correct(corr_baro, dt, z_est, 0, params.w_z_baro);
|
||||
inertial_filter_correct(corr_gps[2][0], dt, z_est, 0, w_z_gps_p);
|
||||
|
||||
if (use_gps_z) {
|
||||
epv = fminf(epv, gps.epv);
|
||||
|
||||
inertial_filter_correct(corr_gps[2][0], dt, z_est, 0, w_z_gps_p);
|
||||
}
|
||||
|
||||
if (!(isfinite(z_est[0]) && isfinite(z_est[1]))) {
|
||||
write_debug_log("BAD ESTIMATE AFTER Z CORRECTION", dt, x_est, y_est, z_est, x_est_prev, y_est_prev, z_est_prev, acc, corr_gps, w_xy_gps_p, w_xy_gps_v);
|
||||
@@ -832,11 +887,15 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
|
||||
|
||||
/* inertial filter correction for position */
|
||||
if (use_flow) {
|
||||
eph = fminf(eph, eph_flow);
|
||||
|
||||
inertial_filter_correct(corr_flow[0], dt, x_est, 1, params.w_xy_flow * w_flow);
|
||||
inertial_filter_correct(corr_flow[1], dt, y_est, 1, params.w_xy_flow * w_flow);
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||||
}
|
||||
|
||||
if (use_gps_xy) {
|
||||
eph = fminf(eph, gps.eph);
|
||||
|
||||
inertial_filter_correct(corr_gps[0][0], dt, x_est, 0, w_xy_gps_p);
|
||||
inertial_filter_correct(corr_gps[1][0], dt, y_est, 0, w_xy_gps_p);
|
||||
|
||||
@@ -910,8 +969,25 @@ int position_estimator_inav_thread_main(int argc, char *argv[])
|
||||
}
|
||||
}
|
||||
|
||||
if (t > pub_last + pub_interval) {
|
||||
if (t > pub_last + PUB_INTERVAL) {
|
||||
pub_last = t;
|
||||
|
||||
/* push current estimate to buffer */
|
||||
est_buf[buf_ptr][0][0] = x_est[0];
|
||||
est_buf[buf_ptr][0][1] = x_est[1];
|
||||
est_buf[buf_ptr][1][0] = y_est[0];
|
||||
est_buf[buf_ptr][1][1] = y_est[1];
|
||||
est_buf[buf_ptr][2][0] = z_est[0];
|
||||
est_buf[buf_ptr][2][1] = z_est[1];
|
||||
|
||||
/* push current rotation matrix to buffer */
|
||||
memcpy(R_buf[buf_ptr], att.R, sizeof(att.R));
|
||||
|
||||
buf_ptr++;
|
||||
if (buf_ptr >= EST_BUF_SIZE) {
|
||||
buf_ptr = 0;
|
||||
}
|
||||
|
||||
/* publish local position */
|
||||
local_pos.xy_valid = can_estimate_xy;
|
||||
local_pos.v_xy_valid = can_estimate_xy;
|
||||
|
||||
@@ -55,6 +55,7 @@ PARAM_DEFINE_FLOAT(INAV_SONAR_ERR, 0.5f);
|
||||
PARAM_DEFINE_FLOAT(INAV_LAND_T, 3.0f);
|
||||
PARAM_DEFINE_FLOAT(INAV_LAND_DISP, 0.7f);
|
||||
PARAM_DEFINE_FLOAT(INAV_LAND_THR, 0.2f);
|
||||
PARAM_DEFINE_FLOAT(INAV_DELAY_GPS, 0.2f);
|
||||
|
||||
int parameters_init(struct position_estimator_inav_param_handles *h)
|
||||
{
|
||||
@@ -73,6 +74,7 @@ int parameters_init(struct position_estimator_inav_param_handles *h)
|
||||
h->land_t = param_find("INAV_LAND_T");
|
||||
h->land_disp = param_find("INAV_LAND_DISP");
|
||||
h->land_thr = param_find("INAV_LAND_THR");
|
||||
h->delay_gps = param_find("INAV_DELAY_GPS");
|
||||
|
||||
return OK;
|
||||
}
|
||||
@@ -94,6 +96,7 @@ int parameters_update(const struct position_estimator_inav_param_handles *h, str
|
||||
param_get(h->land_t, &(p->land_t));
|
||||
param_get(h->land_disp, &(p->land_disp));
|
||||
param_get(h->land_thr, &(p->land_thr));
|
||||
param_get(h->delay_gps, &(p->delay_gps));
|
||||
|
||||
return OK;
|
||||
}
|
||||
|
||||
@@ -56,6 +56,7 @@ struct position_estimator_inav_params {
|
||||
float land_t;
|
||||
float land_disp;
|
||||
float land_thr;
|
||||
float delay_gps;
|
||||
};
|
||||
|
||||
struct position_estimator_inav_param_handles {
|
||||
@@ -74,6 +75,7 @@ struct position_estimator_inav_param_handles {
|
||||
param_t land_t;
|
||||
param_t land_disp;
|
||||
param_t land_thr;
|
||||
param_t delay_gps;
|
||||
};
|
||||
|
||||
/**
|
||||
|
||||
Reference in New Issue
Block a user