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LP-609 Add G force stats and alternate G force / speed/dist max status display
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@ -180,18 +180,19 @@ typedef struct {
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// Private structures
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struct telemetrydata {
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HoTTBridgeSettingsData Settings;
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AttitudeStateData Attitude;
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BaroSensorData Baro;
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AttitudeStateData Attitude;
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AccelStateData Accel;
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BaroSensorData Baro;
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FlightBatteryStateData Battery;
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FlightStatusData FlightStatus;
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FlightStatusData FlightStatus;
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GPSPositionSensorData GPS;
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AirspeedStateData Airspeed;
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AirspeedStateData Airspeed;
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GPSTimeData GPStime;
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GyroSensorData Gyro;
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HomeLocationData Home;
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PositionStateData Position;
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SystemAlarmsData SysAlarms;
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VelocityStateData Velocity;
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GyroSensorData Gyro;
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HomeLocationData Home;
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PositionStateData Position;
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SystemAlarmsData SysAlarms;
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VelocityStateData Velocity;
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int16_t climbratebuffer[climbratesize];
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uint8_t climbrate_pointer;
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float altitude;
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@ -205,6 +206,9 @@ struct telemetrydata {
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float homecourse;
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float max_distance;
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float max_speed;
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float current_G; // G force
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float max_G;
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float min_G;
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uint8_t last_armed;
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char statusline[statussize];
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};
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@ -39,6 +39,7 @@
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#include "callbackinfo.h"
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#include "hottbridgesettings.h"
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#include "attitudestate.h"
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#include "accelstate.h"
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#include "barosensor.h"
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#include "flightbatterystate.h"
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#include "flightstatus.h"
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@ -1289,6 +1290,9 @@ void update_telemetrydata()
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if (AttitudeStateHandle() != NULL) {
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AttitudeStateGet(&telestate->Attitude);
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}
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if (AccelStateHandle() != NULL) {
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AccelStateGet(&telestate->Accel);
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}
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if (BaroSensorHandle() != NULL) {
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BaroSensorGet(&telestate->Baro);
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}
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@ -1325,14 +1329,19 @@ void update_telemetrydata()
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// send actual climbrate value to ring buffer as mm per 0.2s values
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uint8_t n = telestate->climbrate_pointer;
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// DEBUG_PRINTF(3, "Current pointer: %d\r\n", n);
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telestate->climbratebuffer[telestate->climbrate_pointer++] = -telestate->Velocity.Down * 200;
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telestate->climbrate_pointer %= climbratesize;
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// DEBUG_PRINTF(3, "Next pointer: %d\r\n", telestate->climbrate_pointer);
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bool display_G = (n > 25);
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// calculate avarage climbrates in meters per 1, 3 and 10 second(s) based on 200ms interval
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telestate->climbrate1s = 0;
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telestate->climbrate3s = 0;
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telestate->climbrate10s = 0;
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for (uint8_t i = 0; i < climbratesize; i++) {
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// DEBUG_PRINTF(3, "%d ", n);
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telestate->climbrate1s += (i < 5) ? telestate->climbratebuffer[n] : 0;
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telestate->climbrate3s += (i < 15) ? telestate->climbratebuffer[n] : 0;
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telestate->climbrate10s += (i < 50) ? telestate->climbratebuffer[n] : 0;
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@ -1364,6 +1373,10 @@ void update_telemetrydata()
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// calculate current 3D speed
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float speed_3d = sqrtf((telestate->Velocity.North * telestate->Velocity.North) + (telestate->Velocity.East * telestate->Velocity.East) + (telestate->Velocity.Down * telestate->Velocity.Down)) * MS_TO_KMH;
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// Normal Acceleration (G unit)
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float nz_alpha = 0.7f;
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telestate->current_G = ((1 - nz_alpha) * (-telestate->Accel.z / 9.81f)) + (telestate->current_G * nz_alpha);
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// check and set min/max values when armed
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// and without receiver input for standalone board used as sensor
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if ((telestate->FlightStatus.Armed == FLIGHTSTATUS_ARMED_ARMED) || ((telestate->SysAlarms.Alarm.Attitude == SYSTEMALARMS_ALARM_OK) && (telestate->SysAlarms.Alarm.Receiver != SYSTEMALARMS_ALARM_OK))) {
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@ -1379,6 +1392,12 @@ void update_telemetrydata()
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if (telestate->max_speed < speed_3d) {
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telestate->max_speed = speed_3d;
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}
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if (telestate->max_G < telestate->current_G) {
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telestate->max_G = telestate->current_G;
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}
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if (telestate->min_G > telestate->current_G) {
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telestate->min_G = telestate->current_G;
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}
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}
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// statusline
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@ -1488,6 +1507,9 @@ void update_telemetrydata()
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snprintf(telestate->statusline, sizeof(telestate->statusline), "Max %3dkmh Dst %4dm", (uint16_t)telestate->max_speed, (uint16_t)telestate->max_distance);
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// "Max 200kmh"
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// "Dst 1000m "
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if (display_G) {
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snprintf(telestate->statusline, sizeof(telestate->statusline), "MaxG %2d.%d MinG %2d.%d", (int8_t)(telestate->max_G), (int8_t)(telestate->max_G * 10) % 10, (int8_t)(telestate->min_G), (int8_t)abs(telestate->min_G * 10) % 10);
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}
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}
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/**
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