Witamy ponownie
Zaloguj się do swojego konta Altimeter Cloud
Nie masz konta? Utwórz konto
Utwórz darmowe konto
Wyślemy link potwierdzający na Twój e-mail. Sprawdź folder spam, jeśli go nie otrzymasz.
Masz już konto? Zaloguj się
Strona główna
Urządzenie: 1000-3BF4-4BE
Lot ID: 1719200Hz Nano test (1)
Podsumowanie lotu
Wysokość
Apogeum
148.13 Metry
Czas do apogeum
4.44 seconds
Wysokość wypalenia
53.97 m
Wys. maks. prędkości
50.18 m
Wys. wyrzutu
147.97 m
Wys. lądowania
112.3 m
Stabilność
Wskaźnik stabilności
20.2 / 100 (Słaby)
Nachylenie przy wypaleniu (20%)82.5
Prędkość pochylania/odchylania (30%)11.2
Coning · boost (25%)3.8
Prostoliniowość ciągu (15%)0
Launch tilt 6.9° · Coning 281.4/502.6°/s · Spin 204.5°/s · Thrust 77.8%
⚠ Low confidence — altimeter may have moved in flight
About this score
Worked out from the flight log between liftoff and 80% of apogee, independent of the angle the altimeter was mounted at in the airframe.
Nachylenie przy wypaleniu (20%) – how close to vertical it left the rod.
Prędkość pochylania/odchylania (30%) and Coning · boost (25%) – how much the nose swung off the rocket's own axis. The main factor.
Prostoliniowość ciągu (15%) – how cleanly the motor pushed along the body.
Spin about the rocket's own axis is not counted against it — a fast, straight spin is stable. The line under the bars shows the raw measurements.
Prędkość
Maks. wznoszenie
52.72 m/s
Maks. opadanie
-21.55 m/s
Przy wypaleniu
51.280 m/s
Prędk. lądowania
-6.063 m/s
Prędk. opadania
-4.769 m/s
Prędk. wyrzutu
-0.62 m/s
Recovery
Single deploy (no dual deploy detected)
Przyspieszenie
Maks. wznoszenie
8.63 G
Maks. opadanie
42.8 G
Maks. podczas spalania
8.63 G
Śr. wznoszenie
-0.5 G
Śr. spalanie
0.84 G
Czasy
Wypalenie (pierwszy)
0.49 seconds
Apogeum
4.44 seconds
Možliwy wyrzut
4.717 seconds
Lądowanie
11.94 seconds
Kąty
Nachylenie rampy
19.89°
Thrust calc pad tilt
6.9°
Maks. nachylenie do wypalenia
48.59°
Przechylenie startowe
-15.12°
Pochylenie startowe
-9.73°
Maks. obrót (spal.)
1260.33 dps
Śr. obrót (spal.)
678.92 dps
Ogólne
Data przesłania
08/06/26-21:20:10
Próbki danych
5871
Całkowity czas nagrania
42.228 s
Śr. próbki/s
139
Liczba blokad
0
Wysokość nagrywania
81.03 m
Start po włączeniu
1m 4s
Oś referencyjna
X
Bateria & temperatura
Bateria początek
99%
Bateria koniec
96%
Temperatura początek
20.64°C
Temperatura koniec
15.14°C
Animacja danych lotu
FLIGHT 1719
148.13 Meters
ALTITUDE
0.00m
VELOCITY
0.00m/s
ACCEL
0.00G
TILT
0.00°
PITCH
0.00°
ROLL
0.00°
YAW
0.00°
TIME
0.00s
AWAITING LAUNCH
ALT
altimetercloud.com
LAUNCH
T+0.00s
LANDING
BURNOUT
Motor burn complete
Uwaga: Animacja lotu wymaga montażu wysokościomierza w stałej orientacji. Skalibruj czujniki dla najlepszych wyników.
Notatki užytkownika
First test of the Nano altimeter at 200Hz for the new firmware. A small bug on the launch point look back but otherwise has worked rather well. The pre buffer scaling hasn't taken effect so there wasn't enough to have an accurate launch point or lookback, resolved with time based prebuffer rather than fixed sample number.
This flight was flown in the main tube exposed the ejection charge and out in the open air on descent. The True path filter has done a great job at cleaning up the noise and ejection charge pressure spike it would have seen.
This flight was flown in the main tube exposed the ejection charge and out in the open air on descent. The True path filter has done a great job at cleaning up the noise and ejection charge pressure spike it would have seen.
Dodaj to urządzenie do swojego konta, aby edytować
Film Youtube
Brak filmu
Dodaj to urządzenie do swojego konta, aby edytować
Zdjęcia lotu (0)
Brak zdjęć
Powiązana rakieta
✅ Active
1
Klima Pegasus - Test Beast
Klima — Pegasus RTF
✈️ 2 flights linked
Type
Kit build
Diameter
35mm
Length
495mm
Dry weight
80g
Stages
1
Recovery
Parachute
Informacje o urządzeniu
Nano V1
Ten lot został wykonany na Nano V1.
Wersja sprzętu
Rev 4
Wersja oprogramowania
1.52
Ostatnio online
08/06/26-21:20:10
Czujnik ciśnienia
Bosch BMP 581
Akcelerometr
32G 3-axis
Gyroskop
2000 dgps 3-axis
Silniki lotu
1st Stage
1x
Klima
C6-5
Burn time
1.60 seconds
Diameter
18.00 mm
Average thrust
6.00 N
Max thrust
15.00 N
Impulse
10.00 Ns
Impulse class
C
Total weight
20.50 g
Propellant weight
9.60 g
Propellant type
composite
Links
Dodaj to urządzenie do swojego konta, aby edytować
Spalanie silnika
The dashed line is the combined thrust curve for your motors (data from thrustcurve.org), scaled so its peak matches the recorded acceleration maximum — the shape is meaningful, the absolute level is not (your rocket's weight is unknown).
Miejsce startu, data i godzina
Kliknij na mapę, aby oznaczyć miejsce startu. Przełączaj między widokiem mapy i satelity.
No results found — try a different search.
Kliknij na mapę · Przeciągnij, aby dostosować
Lat—
Lng—
✓ Launch location saved successfully.
✗ Could not save location — please try again.
Porównanie lotów
Comparing against 13 other flights with the same motor configuration.
Highest apogee148.13 m 6th of 11
The maximum altitude reached above the launch point.
you
best
best 199.39 m · Flight #1246
Best stability20.2 /100 11th of 11
How straight it flew: launch, coning and thrust straightness combined. 100 is perfect.
you
best
best 93.5 /100 · Flight #1360
Fastest velocity52.72 m/s 4th of 11
Peak ascent velocity recorded during the flight.
you
best
best 61.1 m/s · Flight #1146
Best avg burn G2.68 G 9th of 11
Average acceleration during the motor burn, in G.
you
best
best 3.56 G · Flight #1246
Longest flight42.22 s 4th of 11
Total recording time from launch to landing.
you
best
best 52.3 s · Flight #1333
Lowest spin678.92 dps 11th of 11
Average spin rate during the burn.
you
best
best 53.82 dps · Flight #1333
🌲 Is it in a tree?112.3 m 5th of 11
Just for fun: whichever flight came down closest to 8 m above the launch point (roughly tree height) is the one most likely stuck up a tree.
8 m
you
best
closest to 8 m · 200Hz Nano test (2) (#1734) at 2.38 m
Ogólne ustawienia lotu
To jest migawka ustawień użytych dla tego lotu. Przejdź na
Przejdź na stronę Moje urządzenia i skonfiguruj ustawienia..
Ciśnienie prognozowane
i
Set this to your local forecast pressure at sea level. This will offer you slightly improved accuracty for your flight, although it's not 100% essential every little helps!
Xcweather.co.uk is a decent place to grab pressures from for your location and time.
Xcweather.co.uk is a decent place to grab pressures from for your location and time.
1013.2 mbar
Detekcja startu
i
This is the altitude above the launch pad altitude where the altimeter will trigger itself into recording / flight mode.
The altimeter keeps a constant average of the pressure while waiting for launch, it uses a simple algorithm and the pre-flight buffers to do this. The most recent 120 samples (~4 seconds) are ignored so your pre-trigger altitude won't effect the ground baseline.
For almost all uses we suggest keeping this on the 25 Meter (~82 feet) default settings. If you want to test your altimeter by throwing it in the air, or are planning a very low flight you may want to lower the setting.
The altimeter keeps a constant average of the pressure while waiting for launch, it uses a simple algorithm and the pre-flight buffers to do this. The most recent 120 samples (~4 seconds) are ignored so your pre-trigger altitude won't effect the ground baseline.
For almost all uses we suggest keeping this on the 25 Meter (~82 feet) default settings. If you want to test your altimeter by throwing it in the air, or are planning a very low flight you may want to lower the setting.
30 meters
Sample ratio
i
The altimeter runs at 50Hz however you can record every sample or every X samples in order to extend the log time. For example if you set the ratio to 1 it will save 1:1 samples, or if you set it to 3 it will save 1 in 3 samples.
1:1 (50Hz)
Max samples
i
This is the maximum samples the altimeter will log per flight. When it reaches this amount it will stop and save the recording.
0
Recording stop
i
This setting is how the altimeter decides to stop recording. You can choose either 450 (~9s) or 900 (~18s) samples stable or it will record until the max samples limit unless you press the BUTTON in Manual stop mode.
The samples stable method waits for the devices altitude not to change for the set number of samples. This is defined by not changing by more than +/- 1.0 meters for 98% of the samples, it's a reliable method to stop the recording after landing within 8-10 seconds (300 sample) or 16-20 seconds (600 sample).
The samples stable method waits for the devices altitude not to change for the set number of samples. This is defined by not changing by more than +/- 1.0 meters for 98% of the samples, it's a reliable method to stop the recording after landing within 8-10 seconds (300 sample) or 16-20 seconds (600 sample).
Auto: 450 samples stable (~9s)
Oversampling
i
Oversampling is a internal setting of the BMP 390 pressure sensor. It is how many samples are taken for each reading. By taking multiple samples for each pressure reading the altimeter reduces noise and increases the resolution of the output.
The sensor can run at 50 samples per second in 4X mode, so we suggest leaving it in this mode as it will offer the highest accuracy.
The sensor can run at 50 samples per second in 4X mode, so we suggest leaving it in this mode as it will offer the highest accuracy.
16x Oversampling
IIR filter
i
The IIR filter is another internal sensor for the BMP390 pressure sensor. It is a Infinite impulse response filter used to enhance pressure measurement accuracy by reducing noise. It's primarily for smoothing out rapid pressure changes.
We suggest not setting this too high as it will cause delay to changes in altitude if set very high.
We suggest not setting this too high as it will cause delay to changes in altitude if set very high.
COEFF 7
Pressure filter
i
This filter is a software Kalman filter that runs on the altimeters processor.
The Kalman filter uses a prediction step based on a system model and then a correction step using new measurements to refine its estimate, it creates accurate most certain results from data with noise in it.
The Kalman filter uses a prediction step based on a system model and then a correction step using new measurements to refine its estimate, it creates accurate most certain results from data with noise in it.
TruePath 1.0
Sample speed
i
The sample rate of the altimeter's sensors. 50Hz takes 50 samples per second, 100Hz takes 100 samples per second for higher resolution data.
200 Hz
Hybrid mode
i
When enabled, the altimeter records at full speed during ascent then switches to half speed after apogee to extend recording time during descent.
Enabled
Sync sensors
i
The filters on the pressure sensor can cause it to lag very slightly behind the Accelerometer and Gyroscope data.
The Sync sensors option detects how far out of sync these sensors are. It then corrects the Acceleration and Gyroscope readings to match the pressure sensor.
WŁĄCZONY
Orientation
i
This is the orientation you intend to install the Altimeter in your rocket. It's needed to ensure completly accurate angles and orientation charts and reports. Check out the Manual for more information on this.
Down (text up)
IMU filter
i
The IMU filter, or fusion filter takes the data from each axis of the Gyroscope and Accelerometer to calculate the Pitch, Roll, Yaw and tilt angle from vertical.
These filters can build up some discrepency over time so it's important to calibrate your sensors to minimise this.
Madgwick 6-Axis
Launch ALP
i
This is prevention against accidental launch detection.
With this disabled the launch is based only on pressure and something that creates a low pressure can trigger the flight by accident. For example pulling your nose cone off can even trigger it.
With this enabled the rocket also needs to have seen 8 samples (0.25 seconds) of acceleration above this setting in the last 3 seconds as well as the pressure drop to trigger. There is a backup trigger of 1.05 seconds of altitude being above the launch detect setting too.
There are very few situations where this option would cause issues, so we suggest leaving it on.
With this disabled the launch is based only on pressure and something that creates a low pressure can trigger the flight by accident. For example pulling your nose cone off can even trigger it.
With this enabled the rocket also needs to have seen 8 samples (0.25 seconds) of acceleration above this setting in the last 3 seconds as well as the pressure drop to trigger. There is a backup trigger of 1.05 seconds of altitude being above the launch detect setting too.
There are very few situations where this option would cause issues, so we suggest leaving it on.
1.5G
Launch lock
i
When enabled, the altimeter locks out recording for a set period after power on to prevent false triggering during setup.
DISABLED
Static temperature
i
A fixed temperature value used for altitude calculation when the external temperature sensor is disabled or not connected.
15 °C
Kalibracja czujników
Przesunięcia kalibracji użyte w tym locie.
Gyroskop
X
2.000°
Y
0.000°
Z
0.000°
Akcelerometr
⚠ Akcelerometr nie został skalibrowany
X
0.000 mG
Y
0.000 mG
Z
0.000 mG
Komentarze
Komentarze
Zaloguj się aby komentować.
Zaloguj się aby komentować.