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Dispositivo: 1000-3BF4-4BD8
Vuelo ID: 1209Mostrar eventos
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⚠️
Vuelo de prueba detectado
Esto parece ser un vuelo de prueba o no-cohete (ej. lanzamiento a mano, prueba de vacío/presión). Los datos pueden no representar un vuelo real.
●High altitude with minimal acceleration (vacuum/pressure test)
●No motor burnout detected
●Symmetrical ascent/descent profile
●Gyroscope not responding (all zero readings)
Resumen del vuelo
Altitud
Apogeo
180.27 Metros
Tiempo al apogeo
1.5 seconds
Altitud fin combustión
-4.1 m
Altitud vel. máx.
-9.55 m
Altitud eyección
-4.1 m
Altitud aterrizaje
-8.75 m
Estabilidad
Puntuación estabilidad
0.1 / 100 (Pobre)
Desglose de estabilidad
Inclinación al apagado (20%)0
Constancia de inclinación (15%)0
Cabeceo/guiñada (30%)0
Amortiguación (20%)0
Rectitud de empuje (15%)0
Velocidad
Máx. ascenso
523.92 m/s
Máx. descenso
0 m/s
En fin combustión
0.000 m/s
Vel. aterrizaje
1016.993 m/s
Vel. descenso
1018.115 m/s
Vel. eyección
1020.835490 m/s
Recovery
Single deploy (no dual deploy detected)
Aceleración
Máx. ascenso
0 G
Máx. descenso
0 G
Máx. durante combustión
0 G
Prom. ascenso
0 G
Prom. combustión
0 G
Tiempos
Fin combustión (primero)
0 seconds
Apogeo
1.5 seconds
Posible eyección
0 seconds
Aterrizaje
3.48 seconds
Ángulos
Inclinación rampa
0.00°
Incl. máx. hasta fin comb.
0.00°
Alabeo al lanzamiento
0.00°
Cabeceo al lanzamiento
0.00°
Giro máx. (comb.)
0 dps
Giro prom. (comb.)
0 dps
General
Fecha subida
07/03/26-21:11:09
Muestras de datos
592
Tiempo total grabación
12.054 s
Prom. muestras/s
49.1
Número de bloqueos
0
Altitud grabación
m
Lanzamiento tras encendido
0s
Eje de referencia
Batería & temperatura
Batería inicio
100%
Batería fin
100%
Temperatura inicio
0°C
Temperatura fin
0°C
Animación de datos
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
Nota: La animación de vuelo requiere que su altímetro esté montado en una orientación fija. Calibre sus sensores para mejores resultados.
Notas del usuario
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Vídeo Youtube
Sin vídeo
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Imágenes del vuelo (0)
Sin imágenes
Cohete vinculado
Ningún cohete vinculado a este vuelo
Información del dispositivo
Nano V1
Este vuelo se realizó con un Nano V1.
Versión hardware
Rev 8
Versión software
1.43b
Última conexión
07/03/26-21:11:09
Sensor presión
Bosch BMP 581
Acelerómetro
32G 3-axis
Giroscopio
2000 dgps 3-axis
Motores del vuelo
No se han añadido motores a este vuelo
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Sitio de lanzamiento, fecha y hora
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Lat—
Lng—
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Combustión del motor
Esta es la magnitud de salida del acelerómetro desde el lanzamiento hasta el fin de combustión.
You can check this against your motors thrust data on thrustcurve.org.
Ajustes generales del vuelo
Esta es una captura de los ajustes utilizados para este vuelo. Visite la
Visite la página Mis dispositivos y configure los ajustes..
Presión prevista
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
Detección lanzamiento
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.
DESACTIVADO
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
Calibración de sensores
Compensaciones de calibración usadas en este vuelo.
Giroscopio
⚠ El giroscopio no ha sido calibrado
X
0.000°
Y
0.000°
Z
0.000°
Acelerómetro
⚠ El acelerómetro no ha sido calibrado
X
0.000 mG
Y
0.000 mG
Z
0.000 mG
Comentarios
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