/**************************************************************************** * * Copyright (C) 2012 PX4 Development Team. All rights reserved. * Author: @author Simon Wilks * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions * are met: * * 1. Redistributions of source code must retain the above copyright * notice, this list of conditions and the following disclaimer. * 2. Redistributions in binary form must reproduce the above copyright * notice, this list of conditions and the following disclaimer in * the documentation and/or other materials provided with the * distribution. * 3. Neither the name PX4 nor the names of its contributors may be * used to endorse or promote products derived from this software * without specific prior written permission. * * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE * POSSIBILITY OF SUCH DAMAGE. * ****************************************************************************/ /** * @file messages.c * */ #include "messages.h" #include #include #include #include #include #include #include #include #include #include #include /* The board is very roughly 5 deg warmer than the surrounding air */ #define BOARD_TEMP_OFFSET_DEG 5 static int _battery_sub = -1; static int _gps_sub = -1; static int _home_sub = -1; static int _sensor_sub = -1; static int _airspeed_sub = -1; static int _esc_sub = -1; static orb_advert_t _esc_pub; struct esc_status_s _esc; static bool _home_position_set = false; static double _home_lat = 0.0d; static double _home_lon = 0.0d; void init_sub_messages(void) { _battery_sub = orb_subscribe(ORB_ID(battery_status)); _gps_sub = orb_subscribe(ORB_ID(vehicle_gps_position)); _home_sub = orb_subscribe(ORB_ID(home_position)); _sensor_sub = orb_subscribe(ORB_ID(sensor_combined)); _airspeed_sub = orb_subscribe(ORB_ID(airspeed)); _esc_sub = orb_subscribe(ORB_ID(esc_status)); } void init_pub_messages(void) { memset(&_esc, 0, sizeof(_esc)); _esc_pub = orb_advertise(ORB_ID(esc_status), &_esc); } void build_gam_request(uint8_t *buffer, size_t *size) { struct gam_module_poll_msg msg; *size = sizeof(msg); memset(&msg, 0, *size); msg.mode = BINARY_MODE_REQUEST_ID; msg.id = GAM_SENSOR_ID; memcpy(buffer, &msg, *size); } void publish_gam_message(const uint8_t *buffer) { struct gam_module_msg msg; size_t size = sizeof(msg); memset(&msg, 0, size); memcpy(&msg, buffer, size); /* announce the esc if needed, just publish else */ if (_esc_pub > 0) { orb_publish(ORB_ID(esc_status), _esc_pub, &_esc); } else { _esc_pub = orb_advertise(ORB_ID(esc_status), &_esc); } // Publish it. _esc.esc_count = 1; _esc.esc_connectiontype = ESC_CONNECTION_TYPE_PPM; _esc.esc[0].esc_vendor = ESC_VENDOR_GRAUPNER_HOTT; _esc.esc[0].esc_rpm = (uint16_t)((msg.rpm_H << 8) | (msg.rpm_L & 0xff)) * 10; _esc.esc[0].esc_temperature = msg.temperature1 - 20; _esc.esc[0].esc_voltage = (uint16_t)((msg.main_voltage_H << 8) | (msg.main_voltage_L & 0xff)); _esc.esc[0].esc_current = (uint16_t)((msg.current_H << 8) | (msg.current_L & 0xff)); } void build_eam_response(uint8_t *buffer, size_t *size) { /* get a local copy of the current sensor values */ struct sensor_combined_s raw; memset(&raw, 0, sizeof(raw)); orb_copy(ORB_ID(sensor_combined), _sensor_sub, &raw); /* get a local copy of the battery data */ struct battery_status_s battery; memset(&battery, 0, sizeof(battery)); orb_copy(ORB_ID(battery_status), _battery_sub, &battery); struct eam_module_msg msg; *size = sizeof(msg); memset(&msg, 0, *size); msg.start = START_BYTE; msg.eam_sensor_id = EAM_SENSOR_ID; msg.sensor_text_id = EAM_SENSOR_TEXT_ID; msg.temperature1 = (uint8_t)(raw.baro_temp_celcius + 20); msg.temperature2 = msg.temperature1 - BOARD_TEMP_OFFSET_DEG; msg.main_voltage_L = (uint8_t)(battery.voltage_v * 10); uint16_t alt = (uint16_t)(raw.baro_alt_meter + 500); msg.altitude_L = (uint8_t)alt & 0xff; msg.altitude_H = (uint8_t)(alt >> 8) & 0xff; /* get a local copy of the airspeed data */ struct airspeed_s airspeed; memset(&airspeed, 0, sizeof(airspeed)); orb_copy(ORB_ID(airspeed), _airspeed_sub, &airspeed); uint16_t speed = (uint16_t)(airspeed.indicated_airspeed_m_s * 3.6f); msg.speed_L = (uint8_t)speed & 0xff; msg.speed_H = (uint8_t)(speed >> 8) & 0xff; msg.stop = STOP_BYTE; memcpy(buffer, &msg, *size); } void build_gam_response(uint8_t *buffer, size_t *size) { /* get a local copy of the ESC Status values */ struct esc_status_s esc; memset(&esc, 0, sizeof(esc)); orb_copy(ORB_ID(esc_status), _esc_sub, &esc); struct gam_module_msg msg; *size = sizeof(msg); memset(&msg, 0, *size); msg.start = START_BYTE; msg.gam_sensor_id = GAM_SENSOR_ID; msg.sensor_text_id = GAM_SENSOR_TEXT_ID; msg.temperature1 = (uint8_t)(esc.esc[0].esc_temperature + 20); msg.temperature2 = 20; // 0 deg. C. uint16_t voltage = (uint16_t)(esc.esc[0].esc_voltage); msg.main_voltage_L = (uint8_t)voltage & 0xff; msg.main_voltage_H = (uint8_t)(voltage >> 8) & 0xff; uint16_t current = (uint16_t)(esc.esc[0].esc_current); msg.current_L = (uint8_t)current & 0xff; msg.current_H = (uint8_t)(current >> 8) & 0xff; uint16_t rpm = (uint16_t)(esc.esc[0].esc_rpm * 0.1f); msg.rpm_L = (uint8_t)rpm & 0xff; msg.rpm_H = (uint8_t)(rpm >> 8) & 0xff; msg.stop = STOP_BYTE; memcpy(buffer, &msg, *size); } void build_gps_response(uint8_t *buffer, size_t *size) { /* get a local copy of the current sensor values */ struct sensor_combined_s raw; memset(&raw, 0, sizeof(raw)); orb_copy(ORB_ID(sensor_combined), _sensor_sub, &raw); /* get a local copy of the battery data */ struct vehicle_gps_position_s gps; memset(&gps, 0, sizeof(gps)); orb_copy(ORB_ID(vehicle_gps_position), _gps_sub, &gps); struct gps_module_msg msg; *size = sizeof(msg); memset(&msg, 0, *size); msg.start = START_BYTE; msg.sensor_id = GPS_SENSOR_ID; msg.sensor_text_id = GPS_SENSOR_TEXT_ID; msg.gps_num_sat = gps.satellites_visible; /* The GPS fix type: 0 = none, 2 = 2D, 3 = 3D */ msg.gps_fix_char = (uint8_t)(gps.fix_type + 48); msg.gps_fix = (uint8_t)(gps.fix_type + 48); /* No point collecting more data if we don't have a 3D fix yet */ if (gps.fix_type > 2) { /* Current flight direction */ msg.flight_direction = (uint8_t)(gps.cog_rad * M_RAD_TO_DEG_F); /* GPS speed */ uint16_t speed = (uint16_t)(gps.vel_m_s * 3.6f); msg.gps_speed_L = (uint8_t)speed & 0xff; msg.gps_speed_H = (uint8_t)(speed >> 8) & 0xff; /* Get latitude in degrees, minutes and seconds */ double lat = ((double)(gps.lat))*1e-7d; /* Set the N or S specifier */ msg.latitude_ns = 0; if (lat < 0) { msg.latitude_ns = 1; lat = abs(lat); } int deg; int min; int sec; convert_to_degrees_minutes_seconds(lat, °, &min, &sec); uint16_t lat_min = (uint16_t)(deg * 100 + min); msg.latitude_min_L = (uint8_t)lat_min & 0xff; msg.latitude_min_H = (uint8_t)(lat_min >> 8) & 0xff; uint16_t lat_sec = (uint16_t)(sec); msg.latitude_sec_L = (uint8_t)lat_sec & 0xff; msg.latitude_sec_H = (uint8_t)(lat_sec >> 8) & 0xff; /* Get longitude in degrees, minutes and seconds */ double lon = ((double)(gps.lon))*1e-7d; /* Set the E or W specifier */ msg.longitude_ew = 0; if (lon < 0) { msg.longitude_ew = 1; lon = abs(lon); } convert_to_degrees_minutes_seconds(lon, °, &min, &sec); uint16_t lon_min = (uint16_t)(deg * 100 + min); msg.longitude_min_L = (uint8_t)lon_min & 0xff; msg.longitude_min_H = (uint8_t)(lon_min >> 8) & 0xff; uint16_t lon_sec = (uint16_t)(sec); msg.longitude_sec_L = (uint8_t)lon_sec & 0xff; msg.longitude_sec_H = (uint8_t)(lon_sec >> 8) & 0xff; /* Altitude */ uint16_t alt = (uint16_t)(gps.alt*1e-3f + 500.0f); msg.altitude_L = (uint8_t)alt & 0xff; msg.altitude_H = (uint8_t)(alt >> 8) & 0xff; /* Get any (and probably only ever one) _home_sub postion report */ bool updated; orb_check(_home_sub, &updated); if (updated) { /* get a local copy of the home position data */ struct home_position_s home; memset(&home, 0, sizeof(home)); orb_copy(ORB_ID(home_position), _home_sub, &home); _home_lat = ((double)(home.lat))*1e-7d; _home_lon = ((double)(home.lon))*1e-7d; _home_position_set = true; } /* Distance from home */ if (_home_position_set) { uint16_t dist = (uint16_t)get_distance_to_next_waypoint(_home_lat, _home_lon, lat, lon); msg.distance_L = (uint8_t)dist & 0xff; msg.distance_H = (uint8_t)(dist >> 8) & 0xff; /* Direction back to home */ uint16_t bearing = (uint16_t)(get_bearing_to_next_waypoint(_home_lat, _home_lon, lat, lon) * M_RAD_TO_DEG_F); msg.home_direction = (uint8_t)bearing >> 1; } } msg.stop = STOP_BYTE; memcpy(buffer, &msg, *size); } void convert_to_degrees_minutes_seconds(double val, int *deg, int *min, int *sec) { *deg = (int)val; double delta = val - *deg; const double min_d = delta * 60.0d; *min = (int)min_d; delta = min_d - *min; *sec = (int)(delta * 10000.0d); }