8.24

Flight telemetry summary

Distance Meters

6591.5 m

Maximum Altitude AGL

45.3 m

Maximum Ground Speed

33.76 m/s

Minimum Battery Percent

52%

Minimum Battery Voltage

13.83 V

Minimum GPS Satellites

25

Maximum GPS HDOP

0.62

Flight Modes

MODE_10

Maximum Distance From Home Meters

365.8 m

Maximum Distance From Home Time

4m 7s

Average Ground Speed

21.83 m/s

Maximum Climb Rate MPS

6.58 m/s

Maximum Descent Rate MPS

-6.2 m/s

Battery Consumed MAH

1529.9 mAh

Battery Consumed Wh

22.61 Wh

Voltage Sag

2.91 V

Maximum Estimated Wind Speed MPS

10.92 m/s

Flight Mode Seconds

MODE_10: 5m 8s

Maximum GForce

5.11 g

Compass Healthy

Yes

EKF Healthy

Yes

Maximum GPS Accuracy Meters

0.76 m

Board Temp Max C

51.9 °C

CPU Load Max Percent

8.7%

Weather at the flight

Source

open-meteo-archive

Sampled At Utc

2026-08-24T09:00Z

Latitude

22.37

Longitude

113.54

Temperature C

29.5 °C

Wind Speed MPS

2.84 m/s

Wind Direction Degrees

194

Wind Direction Cardinal

SSW

Weather Code

53

Weather Description

Drizzle moderate

AI flight report

This was a 5-minute-8-second flight covering 6,592 m, flown entirely in MODE_10 in light drizzle with a 29.5°C ambient temperature and a modest 2.84 m/s breeze from the SSW — none of which appears to have been a limiting factor. The aircraft climbed quickly after a 0:12 takeoff, reaching cruise altitude near 40 m by 0:30 and holding roughly 37–43 m above home for the rest of the flight, topping out at the recorded max altitude of 45 m at 1:20. Speed was brisk throughout, averaging 21.8 m/s with a peak of 33.8 m/s at 2:01, and the drone ranged out to 366 m from home by 4:07 before returning and descending back through 15.8 m by 5:00, ending in what the log flags as a descent phase reaching -6.2 m/s at 5:01.

The standout pattern in this flight is motor 4. At 0:00, before the aircraft was even airborne, the log shows a 770 µs asymmetry between motor 3 and motor 4, and by 0:08–0:09 motor 4 was already pinned near saturation (1942 µs, peaking at 2200 µs at 0:09 with a 916 µs spread across motors — versus an ESC ceiling around 2000 µs). That same motor saturated repeatedly across the flight — 0:48, 1:21, 1:56, 2:46, and 4:37 — each time in the 1900–1922 µs range, and a smaller but still notable 201 µs imbalance between motor 1 and motor 4 reappeared right at the end, 4:58. Alongside this, the flight log recorded a cluster of "impact or hard landing" G-spikes (3.1–3.5 G) at 0:33, 0:48, 0:53, 1:17, 1:22, 1:33, 1:57, 2:46 and 3:09, several of them coinciding with steep-attitude warnings (45–70° from level, the steepest at 1:22, which also lines up with the 3.5 G impact flag at the

Detected flight events

1. 0s — Sustained motor asymmetry: motor 3 1570 µs vs motor 4 800 µs (770 µs spread)

   Sustained motor asymmetry: motor 3 1570 µs vs motor 4 800 µs (770 µs spread)

2. 1s — Flight mode changed to MODE_10

   Flight mode changed to MODE_10. The pilot or autopilot switched control behavior here.

3. 8s — Motor 4 at 1942 µs — near maximum output, little authority left

   Motor 4 at 1942 µs — near maximum output, little authority left

4. 12s — Takeoff (altitude threshold)

   Liftoff at 2 m. The aircraft leaves the ground and starts its climb.

5. 26s — Steep attitude: 47° from level

   Steep attitude: 47° from level

6. 33s — Impact or hard landing: 3.3 G

   Impact or hard landing: 3.3 G

7. 48s — Motor 4 at 1902 µs — near maximum output, little authority left

   Motor 4 at 1902 µs — near maximum output, little authority left

8. 48s — Impact or hard landing: 3.1 G

   Impact or hard landing: 3.1 G

9. 53s — Impact or hard landing: 3.3 G

   Impact or hard landing: 3.3 G

10. 56s — Steep attitude: 45° from level

    Steep attitude: 45° from level

11. 1m 17s — Impact or hard landing: 3.4 G

    Impact or hard landing: 3.4 G

12. 1m 20s — Maximum altitude: 45 m above home

    Maximum altitude: 45 m above home — the highest point of this flight.

13. 1m 21s — Motor 4 at 1922 µs — near maximum output, little authority left

    Motor 4 at 1922 µs — near maximum output, little authority left

14. 1m 22s — Impact or hard landing: 3.5 G

    Impact or hard landing: 3.5 G

15. 1m 29s — Steep attitude: 46° from level

    Steep attitude: 46° from level

16. 1m 33s — Impact or hard landing: 3.3 G

    Impact or hard landing: 3.3 G

17. 1m 56s — Motor 4 at 1908 µs — near maximum output, little authority left

    Motor 4 at 1908 µs — near maximum output, little authority left

18. 1m 57s — Impact or hard landing: 3.1 G

    Impact or hard landing: 3.1 G

19. 2m 0s — Steep attitude: 48° from level

    Steep attitude: 48° from level

20. 2m 1s — Maximum ground speed: 33.8 m/s

    Maximum ground speed: 33.8 m/s — the fastest the aircraft moved over the ground.

21. 2m 38s — Steep attitude: 46° from level

    Steep attitude: 46° from level

22. 2m 46s — Motor 4 at 1910 µs — near maximum output, little authority left

    Motor 4 at 1910 µs — near maximum output, little authority left

23. 2m 46s — Impact or hard landing: 3.5 G

    Impact or hard landing: 3.5 G

24. 3m 9s — Impact or hard landing: 3.1 G

    Impact or hard landing: 3.1 G

25. 3m 28s — Steep attitude: 46° from level

    Steep attitude: 46° from level

26. 4m 6s — Steep attitude: 45° from level

    Steep attitude: 45° from level

27. 4m 36s — Steep attitude: 45° from level

    Steep attitude: 45° from level

28. 4m 37s — Motor 4 at 1912 µs — near maximum output, little authority left

    Motor 4 at 1912 µs — near maximum output, little authority left

29. 4m 58s — Sustained motor asymmetry: motor 1 1523 µs vs motor 4 1322 µs (201 µs spread)

    Sustained motor asymmetry: motor 1 1523 µs vs motor 4 1322 µs (201 µs spread)