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Início
Dispositivo: 9C13-9ECF-53C4
Voo ID: 2617Flight 2617
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Resumo do voo
Altitude
Apogeu
301.81 Metros
Tempo até apogeu
10.48 seconds
Altitude fim combustão
0.19 m
Altitude vel. máx.
59.61 m
Altitude ejeção
0.19 m
Altitude aterragem
300.28 m
Estabilidade
Pontuação estabilidade
0 / 100 (Fraco)
Inclinação no fim da queima (20%)0
Taxa arfagem/guinada (30%)0
Coning · boost (25%)0
Retidão de empuxo (15%)0
Launch tilt 0° · Coning 0/0°/s · Spin 0°/s · Thrust 0%
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.
Inclinação no fim da queima (20%) – how close to vertical it left the rod.
Taxa arfagem/guinada (30%) and Coning · boost (25%) – how much the nose swung off the rocket's own axis. The main factor.
Retidão de empuxo (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.
Velocidade
Máx. subida
334.69 m/s
Máx. descida
-266.52 m/s
No fim combustão
2.350 m/s
Vel. aterragem
-4.350 m/s
Vel. descida
234.110 m/s
Vel. ejeção
1.97 m/s
Recovery
Single deploy (no dual deploy detected)
Aceleração
Máx. subida
0.91 G
Máx. descida
3.28 G
Máx. durante combustão
0.05 G
Média subida
0 G
Média combustão
N/A
Tempos
Fim combustão (primeiro)
0 seconds
Apogeu
10.48 seconds
Possível ejeção
0 seconds
Aterragem
9.59 seconds
Saída #1 ON
0 seconds
Saída #1 OFF
0 seconds
Ângulos
Inclinação rampa
86.52°
Thrust calc pad tilt
0°
Incl. máx. até fim comb.
91.51°
Rolagem no lançamento
-80.05°
Arfagem no lançamento
-69.64°
Rotação máx. (comb.)
0 dps
Rotação média (comb.)
0 dps
Geral
Flight time (approx)
No time available
Data envio
15-Jul at 20:37
Amostras de dados
4573
Tempo total gravação
31.500 s
Média amostras/s
145.1
Número de bloqueios
2
Altitude gravação
208.27 m
Lançamento após arranque
6m 56s
Eixo de referência
Z
Bateria & temperatura
Bateria início
94%
Bateria fim
93%
Temperatura início
32.39°C
Temperatura fim
32.45°C
Temp. MT1 lançamento
0°C
Animação dos dados
FLIGHT 2617
301.81 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: A animação de voo requer que o altímetro esteja montado numa orientação fixa. Calibre os sensores para melhores resultados.
Notas do utilizador
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Vídeo Youtube
Sem vídeo
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Imagens do voo (0)
Sem imagens
Foguete associado
Nenhum foguete associado a este voo
Informações do dispositivo
Mercury Plus
Revision 0
Revision 0
Mercury Plus
Este voo foi realizado num Mercury Plus.
Versão hardware
Rev 0
Versão software
1.00
Última ligação
15-Jul at 21:02
Acelerómetro
32G 3-axis
Giroscópio
2000 dgps 3-axis
Sensor pressão
Bosch BMP 390
Magnetómetro
N/A
Motores do voo
Nenhum motor adicionado a este voo
Adicione este dispositivo à sua conta para editar
Combustão do motor
To overlay a thrustcurve here, add your motors to this flight using the “Flight motors” box above. The combined thrust curve is then scaled to match the recorded acceleration peak.
Local de lançamento, data e hora
Clique no mapa para marcar o local de lançamento. Alterne entre vista de mapa e satélite.
No results found — try a different search.
Clique no mapa · Arraste para ajustar
Lat—
Lng—
✓ Launch location saved successfully.
✗ Could not save location — please try again.
Rule events
No output rules fired during this flight.
Correspondência motor (BETA)
Ainda em modo de teste! Estamos a descobrir qual motor foi usado no voo.
Marca
Motor
Pontuação
Forma
Comb.
Estes
1/4A3T
22
1.2%
41.6%
Contrail
G300
18
56%
57%
Definições gerais do voo
Este é um registo das definições utilizadas para este voo. Visite a
Visite a página Meus dispositivos e configure as definições..
Pressão 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.
1018.6 mbar
Deteção lançamento
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.
35 meters
Taxa amostragem
i
The base sample rate of the altimeter's sensors in samples per second. This setting was deprecated in firmware 2.0+.
32 Hz
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.
1:5 (hybrid, reduces after apogee)
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.
18000
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.
Kalman 2 (default)
Lockout change
i
This is how we detect a lockout. If the pressure changes by this much in a single sample downwards (pressure increase, lower altitude) then it's likely to be a false reading. Multiply the setting by 32 to get the speed in meters per second that it will trigger at.
0.5 meters
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.
ATIVADO
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.
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.
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
Temp sensor
i
If an external MT1 temperature sensor is connected, this controls whether it is used for logging only or also for altitude calculations.
DISABLED
Definições de saída
Este é um registo das definições utilizadas para este voo.
Arm switch
i
When enabled, GP6 is a hardware arm switch — outputs and rules are held off until the switch is closed to ground.
DISABLED
Startup lockout
i
Outputs and rules are blocked for this many seconds after power-on while sensors settle. 0 = off.
None
Launch confirm delay
i
After launch is detected, outputs and rules won't fire until this many seconds have passed.
2 s
Altitude floor
i
Outputs and rules are blocked until the rocket is at least this height above the launch pad.
50 m
Custom dataset 1
i
User-defined expression evaluated per sample, available for charting.
—
Custom dataset 2
—
Calibração de sensores
Desvios de calibração utilizados neste voo.
Giroscópio
⚠ O giroscópio não foi calibrado
X
0.000°
Y
0.000°
Z
0.000°
Acelerómetro
⚠ O acelerómetro não foi calibrado
X
0.000 mG
Y
0.000 mG
Z
0.000 mG
Definições do dispositivo
Este é um registo das definições utilizadas para este voo.
Este é um registo das definições utilizadas para este voo.
TAG dispositivo
i
A custom name or tag assigned to this device for easy identification.
Merc9119
Idioma
i
The language setting configured on the device.
🇬🇧 English
Modo encerramento
i
Controls what happens after recording. Standard shuts down normally, Delayed keeps WiFi on for 30 seconds after landing, Stay on keeps the device powered on.
Delayed 30s
Brilho LED
i
The brightness level of the LED indicators on the Mercury. Lower values save battery.
20%
WiFi TX power
i
WiFi transmit power level. Higher gives better range but uses more battery.
2 dBm (low)
Modo suspensão
i
Controls whether the device enters low-power sleep when idle.
Normal (sleep when idle)
Monitor bateria
i
Monitors battery voltage during the flight.
DISABLED
Cloud group
i
The cloud group / category this flight is assigned to.
General use
Portas GP6 / GP7
O controlo de portas GP não estava disponível até o firmware 2.0
Placa servo I2C PCA9685
O controlo de portas GP não estava disponível até o firmware 2.0
Previsão e freios aéreos
Esta funcionalidade não estava disponível até à versão 2.10+
Comentários
Comentários
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