Altimeter cloud: Flight 2618

Definições gerais do voo

Pressão prevista

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.

1018.6 mbar

Deteção lançamento

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.

50 meters

Taxa amostragem

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

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

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

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).

Auto: 450 samples stable (~9s)

Oversampling

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.

16x Oversampling

IIR filter

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.

COEFF 7

Pressure filter

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.

Kalman 2 (default)

Lockout change

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

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 (5 samples / 37.00ms)

Orientation

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

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

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.

1.4G

Launch lock

When enabled, the altimeter locks out recording for a set period after power on to prevent false triggering during setup.

DISABLED

Static temperature

A fixed temperature value used for altitude calculation when the external temperature sensor is disabled or not connected.

15 °C

Temp sensor

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

Arm switch

When enabled, GP6 is a hardware arm switch — outputs and rules are held off until the switch is closed to ground.

DISABLED

Startup lockout

Outputs and rules are blocked for this many seconds after power-on while sensors settle. 0 = off.

None

Launch confirm delay

After launch is detected, outputs and rules won't fire until this many seconds have passed.

2 s

Altitude floor

Outputs and rules are blocked until the rocket is at least this height above the launch pad.

50 m

Custom dataset 1

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

X0.000°

Y0.000°

Z0.000°

Acelerómetro⚠ O acelerómetro não foi calibrado

X0.000 mG

Y0.000 mG

Z0.000 mG

Definições do dispositivo

TAG dispositivo

A custom name or tag assigned to this device for easy identification.

Merc9119

Idioma

The language setting configured on the device.

🇬🇧 English

Modo encerramento

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

The brightness level of the LED indicators on the Mercury. Lower values save battery.

20%

WiFi TX power

WiFi transmit power level. Higher gives better range but uses more battery.

2 dBm (low)

Modo suspensão

Controls whether the device enters low-power sleep when idle.

Normal (sleep when idle)

Monitor bateria

Monitors battery voltage during the flight.

DISABLED

Cloud group

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+

Flight 2618

The flight, moment by moment

Estabilidade0.1%Fraco

Rocket information

About the stability score

Linked flights

Local de lançamento, data e hora

Apogee, adjusted for conditions

FLIGHT 2618

Flights from this altimeter

Settings, as they were for this flight

Files

Apogee, adjusted for conditions

FLIGHT 2618

BURNOUT

Flights from this altimeter

Files

Share this flight

Chart snapshot

Hotlink images

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