feat : caculate inclination among all of waypoints and between starting point and current position
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81 additions
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10 deletions
... | @@ -40,7 +40,7 @@ using math::constrain; | ... | @@ -40,7 +40,7 @@ using math::constrain; |
40 | using matrix::Eulerf; | 40 | using matrix::Eulerf; |
41 | using matrix::Quatf; | 41 | using matrix::Quatf; |
42 | using matrix::Vector3f; | 42 | using matrix::Vector3f; |
43 | - | 43 | +int static hold=0; |
44 | pthread_mutex_t ekf2_module_mutex = PTHREAD_MUTEX_INITIALIZER; | 44 | pthread_mutex_t ekf2_module_mutex = PTHREAD_MUTEX_INITIALIZER; |
45 | static px4::atomic<EKF2 *> _objects[EKF2_MAX_INSTANCES] {}; | 45 | static px4::atomic<EKF2 *> _objects[EKF2_MAX_INSTANCES] {}; |
46 | #if !defined(CONSTRAINED_FLASH) | 46 | #if !defined(CONSTRAINED_FLASH) |
... | @@ -1509,19 +1509,83 @@ void EKF2::UpdateGpsSample(ekf2_timestamps_s &ekf2_timestamps) | ... | @@ -1509,19 +1509,83 @@ void EKF2::UpdateGpsSample(ekf2_timestamps_s &ekf2_timestamps) |
1509 | + vehicle_gps_position.vdop * vehicle_gps_position.vdop), | 1509 | + vehicle_gps_position.vdop * vehicle_gps_position.vdop), |
1510 | }; | 1510 | }; |
1511 | _ekf.setGpsData(gps_msg); | 1511 | _ekf.setGpsData(gps_msg); |
1512 | - mission_s mission; | 1512 | + if(hold != int(gps_msg.time_usec/1000000)) |
1513 | - dm_read(DM_KEY_MISSION_STATE, 0, &mission, sizeof(mission_s)); | 1513 | + { |
1514 | - for (size_t i = 0; i < mission.count; i++) { | 1514 | + dm_read(DM_KEY_MISSION_STATE, 0, &mission, sizeof(mission_s)); |
1515 | - struct mission_item_s mission_item {}; | 1515 | + hold=int(gps_msg.time_usec/1000000); |
1516 | - dm_read((dm_item_t)mission.dataman_id, i, &mission_item, sizeof(mission_item_s)); | 1516 | + if(hold%2==0) |
1517 | - std::cout<<"target\t"<<i<< "(lat/lon/alt)\t" << mission_item.lat << "\t"<<mission_item.lon<<"\t"<<mission_item.altitude<<std::endl; | 1517 | + { |
1518 | + calculate_inclination_target(); | ||
1519 | + print_target_gps(); | ||
1520 | + //print_current_gps(gps_msg); | ||
1521 | + calculate_inclination_current(gps_msg); | ||
1522 | + } | ||
1518 | } | 1523 | } |
1519 | _gps_time_usec = gps_msg.time_usec; | 1524 | _gps_time_usec = gps_msg.time_usec; |
1520 | _gps_alttitude_ellipsoid = vehicle_gps_position.alt_ellipsoid; | 1525 | _gps_alttitude_ellipsoid = vehicle_gps_position.alt_ellipsoid; |
1521 | } | 1526 | } |
1522 | } | 1527 | } |
1523 | } | 1528 | } |
1529 | +void EKF2::print_current_gps(gps_message gps_msg) | ||
1530 | +{ | ||
1531 | + std::cout<<"curre\t#"<<mission.current_seq<<"(lat/lon/alt)\t" << gps_msg.lat << "\t"<<gps_msg.lon<<"\t"<<gps_msg.alt<<std::endl; | ||
1532 | +} | ||
1533 | +void EKF2::calculate_inclination_target() | ||
1534 | +{ | ||
1535 | + double x,y; | ||
1536 | + inclination=new double[int(mission.count)]; | ||
1537 | + for (size_t i = 0; i < mission.count-1; i++) { | ||
1538 | + struct mission_item_s mission_item {}; | ||
1539 | + struct mission_item_s next_mission_item {}; | ||
1540 | + dm_read((dm_item_t)mission.dataman_id, i, &mission_item, sizeof(mission_item_s)); | ||
1541 | + dm_read((dm_item_t)mission.dataman_id, i+1, &next_mission_item, sizeof(mission_item_s)); | ||
1542 | + //std:: cout << "next : "<<next_mission_item.lat<<std::endl; | ||
1543 | + //std:: cout << "curr : "<<mission_item.lat<<std::endl; | ||
1544 | + x=next_mission_item.lat-mission_item.lat; | ||
1545 | + y=next_mission_item.lon-mission_item.lon; | ||
1546 | + std::cout.setf(std::ios::fixed); | ||
1547 | + std::cout.precision(7); | ||
1548 | + if(x!=0.0){ | ||
1549 | + inclination[i]=y/x; | ||
1550 | + } | ||
1551 | + else | ||
1552 | + { | ||
1553 | + inclination[i]=0.0; | ||
1554 | + } | ||
1555 | + /*if(int(i)==int(mission.current_seq)-1){ | ||
1556 | + std::cout <<"[inclina]#"<<i<<"\t"<<inclination[i]<<std::endl; | ||
1557 | + }*/ | ||
1558 | + } | ||
1559 | +} | ||
1560 | +void EKF2::calculate_inclination_current(gps_message gps_msg) | ||
1561 | +{ | ||
1562 | + double x,y; | ||
1563 | + double check_inclination=0; | ||
1564 | + x=target_lat-gps_msg.lat; | ||
1565 | + y=target_lon-gps_msg.lon; | ||
1566 | + if(x!=0.0){ | ||
1567 | + check_inclination=y/x; | ||
1568 | + } | ||
1569 | + std::cout.setf(std::ios::fixed); | ||
1570 | + std::cout.precision(7); | ||
1571 | + std::cout << "[Mission] #"<<mission.current_seq<<"\t"<<check_inclination<<std::endl; | ||
1524 | 1572 | ||
1573 | +} | ||
1574 | +void EKF2::print_target_gps() | ||
1575 | +{ | ||
1576 | + std::cout.unsetf(std::ios::fixed); | ||
1577 | + | ||
1578 | + for (size_t i = 0; i < mission.count; i++) { | ||
1579 | + struct mission_item_s mission_item {}; | ||
1580 | + if(int(mission.current_seq)==int(i)){ | ||
1581 | + dm_read((dm_item_t)mission.dataman_id, i, &mission_item, sizeof(mission_item_s)); | ||
1582 | + target_lat=int32_t(mission_item.lat * long(pow(10,7))); | ||
1583 | + target_lon=int32_t(mission_item.lon * long(pow(10,7))); | ||
1584 | + target_alt=int32_t(mission_item.altitude * long(pow(10,4))); | ||
1585 | + //std::cout<<"start\t#"<<i<< "(lat/lon/alt)\t" << target_lat<< "\t"<<target_lon<<"\t"<<target_alt<<std::endl; | ||
1586 | + } | ||
1587 | + } | ||
1588 | +} | ||
1525 | void EKF2::UpdateMagSample(ekf2_timestamps_s &ekf2_timestamps) | 1589 | void EKF2::UpdateMagSample(ekf2_timestamps_s &ekf2_timestamps) |
1526 | { | 1590 | { |
1527 | const unsigned last_generation = _magnetometer_sub.get_last_generation(); | 1591 | const unsigned last_generation = _magnetometer_sub.get_last_generation(); | ... | ... |
... | @@ -43,7 +43,7 @@ | ... | @@ -43,7 +43,7 @@ |
43 | #include "EKF2Selector.hpp" | 43 | #include "EKF2Selector.hpp" |
44 | 44 | ||
45 | #include <float.h> | 45 | #include <float.h> |
46 | - | 46 | +#include <dataman/dataman.h> |
47 | #include <containers/LockGuard.hpp> | 47 | #include <containers/LockGuard.hpp> |
48 | #include <drivers/drv_hrt.h> | 48 | #include <drivers/drv_hrt.h> |
49 | #include <lib/ecl/EKF/ekf.h> | 49 | #include <lib/ecl/EKF/ekf.h> |
... | @@ -155,14 +155,19 @@ private: | ... | @@ -155,14 +155,19 @@ private: |
155 | void UpdateRangeSample(ekf2_timestamps_s &ekf2_timestamps); | 155 | void UpdateRangeSample(ekf2_timestamps_s &ekf2_timestamps); |
156 | 156 | ||
157 | void UpdateMagCalibration(const hrt_abstime ×tamp); | 157 | void UpdateMagCalibration(const hrt_abstime ×tamp); |
158 | - | 158 | + void print_target_gps(); |
159 | + void print_current_gps(gps_message gps_msg); | ||
160 | + void calculate_inclination_target(); | ||
161 | + void calculate_inclination_current(gps_message gps_msg); | ||
162 | + double* inclination=nullptr; | ||
163 | + int32_t target_lat,target_lon,target_alt; | ||
164 | + mission_s mission; | ||
159 | /* | 165 | /* |
160 | * Calculate filtered WGS84 height from estimated AMSL height | 166 | * Calculate filtered WGS84 height from estimated AMSL height |
161 | */ | 167 | */ |
162 | float filter_altitude_ellipsoid(float amsl_hgt); | 168 | float filter_altitude_ellipsoid(float amsl_hgt); |
163 | 169 | ||
164 | static constexpr float sq(float x) { return x * x; }; | 170 | static constexpr float sq(float x) { return x * x; }; |
165 | - | ||
166 | const bool _replay_mode{false}; ///< true when we use replay data from a log | 171 | const bool _replay_mode{false}; ///< true when we use replay data from a log |
167 | const bool _multi_mode; | 172 | const bool _multi_mode; |
168 | int _instance{0}; | 173 | int _instance{0}; |
... | @@ -176,6 +181,8 @@ private: | ... | @@ -176,6 +181,8 @@ private: |
176 | 181 | ||
177 | perf_counter_t _ecl_ekf_update_perf{perf_alloc(PC_ELAPSED, MODULE_NAME": ECL update")}; | 182 | perf_counter_t _ecl_ekf_update_perf{perf_alloc(PC_ELAPSED, MODULE_NAME": ECL update")}; |
178 | perf_counter_t _ecl_ekf_update_full_perf{perf_alloc(PC_ELAPSED, MODULE_NAME": ECL full update")}; | 183 | perf_counter_t _ecl_ekf_update_full_perf{perf_alloc(PC_ELAPSED, MODULE_NAME": ECL full update")}; |
184 | + perf_counter_t _imu_missed_perf{perf_alloc(PC_COUNT, MODULE_NAME": IMU message missed")}; | ||
185 | + perf_counter_t _mag_missed_perf{perf_alloc(PC_COUNT, MODULE_NAME": mag message missed")}; | ||
179 | 186 | ||
180 | // Used to check, save and use learned magnetometer biases | 187 | // Used to check, save and use learned magnetometer biases |
181 | hrt_abstime _mag_cal_last_us{0}; ///< last time the EKF was operating a mode that estimates magnetomer biases (uSec) | 188 | hrt_abstime _mag_cal_last_us{0}; ///< last time the EKF was operating a mode that estimates magnetomer biases (uSec) | ... | ... |
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