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Úvod
Zařízení: 1000-3BF4-4BD8
Let ID: 1209Zobrazit události
Stáhnout
Upravit tepl. & tlak ?
Obrázek
Datové sady
Klikněte na legendu pro zobrazení nebo skrytí dat
Přiblížení
Klikněte a táhněte nebo použijte gesto
Porovnat let ?
⚠️
Zjištěn testovací let
Toto se jeví jako testovací nebo neraketový let (např. hod rukou, vakuový/tlakový test). Data nemusí představovat skutečný let rakety.
●High altitude with minimal acceleration (vacuum/pressure test)
●No motor burnout detected
●Symmetrical ascent/descent profile
●Gyroscope not responding (all zero readings)
Shrnutí letu
Výška
Apogeum
180.27 Metry
Čas do apogea
1.5 seconds
Výška vyhoření
-4.1 m
Výška max. rychlosti
-9.55 m
Výška vypuštění
-4.1 m
Výška přistání
-8.75 m
Stabilita
Skóre stability
0.1 / 100 (Špatný)
Rozklad stability
Náklon při dohoření (20%)0
Stálost náklonu (15%)0
Klápění/zatáčení (30%)0
Tlumení (20%)0
Přímost tahu (15%)0
Rychlost
Max. stoupání
523.92 m/s
Max. klesání
0 m/s
Při vyhoření
0.000 m/s
Rychl. přistání
1016.993 m/s
Rychl. klesání
1018.115 m/s
Rychl. vypuštění
1020.835490 m/s
Recovery
Single deploy (no dual deploy detected)
Zrychlení
Max. stoupání
0 G
Max. klesání
0 G
Max. při spalování
0 G
Prúm. stoupání
0 G
Prúm. spalování
0 G
Časy
Vyhoření (první)
0 seconds
Apogeum
1.5 seconds
Možné vypuštění
0 seconds
Přistání
3.48 seconds
Úhly
Náklon rampy
0.00°
Max. náklon do vyhoření
0.00°
Klápění při startu
0.00°
Klopní při startu
0.00°
Max. rotace (spal.)
0 dps
Prúm. rotace (spal.)
0 dps
Obecné
Datum nahrání
07/03/26-21:11:09
Datové vzorky
592
Celkový čas záznamu
12.054 s
Prúm. vzorký/s
49.1
Počet blokování
0
Výška záznamu
m
Start po zapnutí
0s
Referenční osa
Baterie & teplota
Baterie začátek
100%
Baterie konec
100%
Teplota začátek
0°C
Teplota konec
0°C
Animace dat letu
FLIGHT 1209
180.27 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
Poznámka: Animace letu vyžaduje montáž výškoměru v pevné orientaci. Kalibrujte senzory pro nejlepší výsledky.
Uživatelské poznámky
Přidejte toto zařízení ke svému účtu pro úpravy
Youtube video
Žádné video
Přidejte toto zařízení ke svému účtu pro úpravy
Obrázky letu (0)
Žádné obrázky
Propojená raketa
K tomuto letu není připojena žádná raketa
Informace o zařízení
Nano V1
Tento let byl proveden na Nano V1.
Verze hardware
Rev 8
Verze software
1.43b
Naposledy online
07/03/26-21:11:09
Snímač tlaku
Bosch BMP 581
Akcelerometr
32G 3-axis
Gyroskop
2000 dgps 3-axis
Motory letu
K tomuto letu nebyly přidány žádné motory
Přidejte toto zařízení ke svému účtu pro úpravy
Místo startu, datum a čas
Klikněte na mapu pro označení místa startu. Přepínejte mezi mapou a satelitním pohledem.
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Klikněte na mapu · Přetáhněte pro úpravu
Lat—
Lng—
✓ Launch location saved successfully.
✗ Could not save location — please try again.
Spalování motoru
Toto je velikost výstupu akcelerometru od startu do vyhoření.
You can check this against your motors thrust data on thrustcurve.org.
Obecná nastavení letu
Toto je snímek nastavení použitých pro tento let. Přejděte na
Přejděte na stránku Moje zařízení a nakonfigurujte nastavení..
Předpovězený tlak
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
Detekce 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.
25 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.
35000
Recording stop
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
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.
Kalman 1 (less)
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.
DEAKTIVOVÁNO
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.
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
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.
Disabled
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
Kalibrace senzorú
Kalibrační offsety použité pro tento let.
Gyroskop
⚠ Gyroskop nebyl zkalibrován
X
0.000°
Y
0.000°
Z
0.000°
Akcelerometr
⚠ Akcelerometr nebyl zkalibrován
X
0.000 mG
Y
0.000 mG
Z
0.000 mG
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