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Startseite
Gerät: 1000-3BF4-4BD8
Flug-ID: 1208⚠️
Testflug erkannt
Dies scheint ein Test- oder Nicht-Raketenflug zu sein (z.B. Handwurf, Vakuum-/Drucktest). Die Daten stellen möglicherweise keinen echten Raketenflug dar.
●Extremely short flight (under 3 seconds)
●High altitude with minimal acceleration (vacuum/pressure test)
●Reached high altitude impossibly fast
●No motor burnout detected
●Gyroscope not responding (all zero readings)
Flugzusammenfassung
Höhe
Apogäum
45.33 Meter
Zeit bis Apogäum
0.59 seconds
Brennschluss-Höhe
0.5 m
Max. Geschw.-Höhe
-2.16 m
Auswurf-Höhe
0.5 m
Lande-Höhe
0.16 m
Stabilität
Stabilitätswert
0.1 / 100 (Schlecht)
Stabilitätsaufschlüsselung
Neigung bei Brennschluss (20%)0
Neigungskonstanz (15%)0
Nick/Gier-Rate (30%)0
Dämpfung (20%)0
Schubgeradheit (15%)0
Geschwindigkeit
Max. Aufstieg
111.94 m/s
Max. Abstieg
0 m/s
Bei Brennschluss
0.000 m/s
Landegeschw.
1020.881 m/s
Abstiegsgeschw.
1020.995 m/s
Auswurfgeschw.
1021.370862 m/s
Recovery
Single deploy (no dual deploy detected)
Beschleunigung
Max. Aufstieg
0 G
Max. Abstieg
0 G
Max. während Brennen
0 G
Durchschn. Aufstieg
0 G
Durchschn. Brennen
0 G
Zeiten
Brennschluss (erster)
0 seconds
Apogäum
0.59 seconds
Möglicher Auswurf
0 seconds
Landung
2.9 seconds
Winkel
Rampen-Neigung
0.00°
Max. Neigung bis Brennschluss
0.00°
Start-Roll
0.00°
Start-Nick
0.00°
Max. Drehung (Brennen)
0 dps
Durchschn. Drehung (Brennen)
0 dps
Allgemein
Upload-Datum
07/03/26-21:10:31
Datenpunkte
810
Gesamte Aufnahmezeit
16.446 s
Durchschn. Abtastrate/s
49.2
Anzahl Sperren
0
Aufnahme-Höhe
m
Start nach Einschalten
0s
Referenzachse
Batterie & Temperatur
Batterie Start
100%
Batterie Ende
100%
Temperatur Start
0°C
Temperatur Ende
0°C
Flugdaten-Animation
FLIGHT 1208
45.33 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
Hinweis: Die Fluganimation erfordert eine feste Ausrichtung Ihres Höhenmessers. Kalibrieren Sie Ihre Sensoren für beste Ergebnisse.
Benutzernotizen
Fügen Sie dieses Gerät Ihrem Konto hinzu, um zu bearbeiten
Youtube-Video
Kein Video
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Flugbilder (0)
Keine Bilder
Verknüpfte Rakete
Keine Rakete mit diesem Flug verknüpft
Geräteinformationen
Nano V1
Dieser Flug wurde mit einem geflogen: Nano V1.
Hardwareversion
Rev 8
Softwareversion
1.43b
Zuletzt online
07/03/26-21:10:31
Drucksensor
Bosch BMP 581
Beschleunigungssensor
32G 3-axis
Gyroskop
2000 dgps 3-axis
Flugmotoren
Keine Motoren zu diesem Flug hinzugefügt
Fügen Sie dieses Gerät Ihrem Konto hinzu, um zu bearbeiten
Startplatz, Datum & Uhrzeit
Klicken Sie auf die Karte, um Ihren Startplatz zu markieren. Wechseln Sie zwischen Karten- und Satellitenansicht.
No results found — try a different search.
Klicken Sie auf die Karte · Ziehen zum Anpassen
Lat—
Lng—
✓ Launch location saved successfully.
✗ Could not save location — please try again.
Motorbrenndauer
Dies ist die Beschleunigungssensor-Gesamtgröße vom Start bis Brennschluss.
You can check this against your motors thrust data on thrustcurve.org.
Allgemeine Flugeinstellungen
Dies ist ein Schnappschuss der für diesen Flug verwendeten Einstellungen. Gehen Sie zur
Gehen Sie zur Meine Geräte Seite und konfigurieren Sie die Einstellungen..
Prognosedruck
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
Starterkennung
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.
25 meters
Abtastverhältnis
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. Abtastungen
i
This is the maximum samples the altimeter will log per flight. When it reaches this amount it will stop and save the recording.
35000
Aufnahme-Stopp
i
This setting is how the altimeter decides to stop recording. You can choose either 300 or 600 samples stable or it will record until it's 10000 sample 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: 300 samples stable
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.
8x 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
Druckfilter
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.
Kalman 1 (less)
Sensorsynchronisation
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.
DEAKTIVIERT
Ausrichtung
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.
Upwards (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.
Mahony 6-Axis
Start-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.
Disabled
Startsperre
i
When enabled, the altimeter locks out recording for a set period after power on to prevent false triggering during setup.
DISABLED
Statische Temperatur
i
A fixed temperature value used for altitude calculation when the external temperature sensor is disabled or not connected.
15 °C
Sensorkalibrierung
Kalibrierungsversätze für diesen Flug.
Gyroskop
⚠ Gyroskop wurde nicht kalibriert
X
0.000°
Y
0.000°
Z
0.000°
Beschleunigungssensor
⚠ Beschleunigungssensor wurde nicht kalibriert
X
0.000 mG
Y
0.000 mG
Z
0.000 mG
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