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Apparaat: 9C13-9ECF-53C4
Vlucht ID: 2617Flight 2617
Toon gebeurtenissen
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Temp. & druk aanpassen ?
Afbeelding
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Klik en sleep, of knijp op mobiel
Vlucht vergelijken ?
Vluchtsamenvatting
Hoogte
Apogeum
301.81 Meter
Tijd tot apogeum
10.48 seconds
Hoogte uitbranding
0.19 m
Hoogte max. snelheid
59.61 m
Hoogte uitwerping
0.19 m
Hoogte landing
300.28 m
Stabiliteit
Stabiliteitsscore
0 / 100 (Slecht)
Helling bij burnout (20%)0
Stamp/gier snelheid (30%)0
Coning · boost (25%)0
Stuwkrachtrechtheid (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.
Helling bij burnout (20%) – how close to vertical it left the rod.
Stamp/gier snelheid (30%) and Coning · boost (25%) – how much the nose swung off the rocket's own axis. The main factor.
Stuwkrachtrechtheid (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.
Snelheid
Max. stijging
334.69 m/s
Max. daling
-266.52 m/s
Bij uitbranding
2.350 m/s
Snelheid landing
-4.350 m/s
Snelheid daling
234.110 m/s
Snelheid uitwerping
1.97 m/s
Recovery
Single deploy (no dual deploy detected)
Versnelling
Max. stijging
0.91 G
Max. daling
3.28 G
Max. tijdens verbranding
0.05 G
Gem. stijging
0 G
Gem. verbranding
N/A
Tijden
Uitbranding (eerste)
0 seconds
Apogeum
10.48 seconds
Mogelijke uitwerping
0 seconds
Landing
9.59 seconds
Uitgang #1 AAN
0 seconds
Uitgang #1 UIT
0 seconds
Hoeken
Helling lanceerplatform
86.52°
Thrust calc pad tilt
0°
Max. helling tot uitbranding
91.51°
Rol bij lancering
-80.05°
Stamp bij lancering
-69.64°
Max. rotatie (verbr.)
0 dps
Gem. rotatie (verbr.)
0 dps
Algemeen
Flight time (approx)
No time available
Uploaddatum
15-Jul at 20:37
Datapunten
4573
Totale opnametijd
31.500 s
Gem. monsters/s
145.1
Aantal vergrendelingen
2
Opnamehoogte
208.27 m
Lancering na inschakelen
6m 56s
Referentie-as
Z
Batterij & temperatuur
Batterij start
94%
Batterij einde
93%
Temperatuur start
32.39°C
Temperatuur einde
32.45°C
Temp. MT1 lancering
0°C
Vluchtdata-animatie
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
Opmerking: De vluchtanimatie vereist dat uw hoogtemeter in een vaste oriëntatie is gemonteerd. Kalibreer uw sensoren voor de beste resultaten.
Gebruikersnotities
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Youtube-video
Geen video
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Vluchtafbeeldingen (0)
Geen afbeeldingen
Gekoppelde raket
Geen raket gekoppeld aan deze vlucht
Apparaatinformatie
Mercury Plus
Revision 0
Revision 0
Mercury Plus
Deze vlucht is gevlogen met een Mercury Plus.
Hardwareversie
Rev 0
Softwareversie
1.00
Laatst online
15-Jul at 21:02
Versnellingsmeter
32G 3-axis
Gyroscoop
2000 dgps 3-axis
Druksensor
Bosch BMP 390
Magnetometer
N/A
Vluchtmotoren
Geen motoren toegevoegd aan deze vlucht
Voeg dit apparaat toe aan uw account om te bewerken
Motorbrandduur
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.
Lanceerplaats, datum & tijd
Klik op de kaart om uw lanceerlocatie te markeren. Schakel tussen kaart- en satellietweergave.
No results found — try a different search.
Klik op de kaart · Sleep om aan te passen
Lat—
Lng—
✓ Launch location saved successfully.
✗ Could not save location — please try again.
Rule events
No output rules fired during this flight.
Motorkoppeling (BETA)
Nog in testmodus! We werken eraan om te bepalen welke motor is gebruikt.
Merk
Motor
Score
Vorm
Brand
Estes
1/4A3T
22
1.2%
41.6%
Contrail
G300
18
56%
57%
Algemene vluchtinstellingen
Dit is een momentopname van de instellingen die voor deze vlucht zijn gebruikt. Ga naar de
Ga naar de pagina Mijn apparaten en configureer de instellingen..
Voorspelde druk
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
Lanceerdetectie
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
Bemonsteringsfrequentie
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.
INGESCHAKELD
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
Uitvoerinstellingen
Dit is een momentopname van de instellingen die voor deze vlucht zijn gebruikt.
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
—
Sensorkalibratie
Kalibratie-offsets gebruikt voor deze vlucht.
Gyroscoop
⚠ Gyroscoop is niet gekalibreerd
X
0.000°
Y
0.000°
Z
0.000°
Versnellingsmeter
⚠ Versnellingsmeter is niet gekalibreerd
X
0.000 mG
Y
0.000 mG
Z
0.000 mG
Apparaatinstellingen
Dit is een momentopname van de instellingen die voor deze vlucht zijn gebruikt.
Dit is een momentopname van de instellingen die voor deze vlucht zijn gebruikt.
Apparaat-TAG
i
A custom name or tag assigned to this device for easy identification.
Merc9119
Taal
i
The language setting configured on the device.
🇬🇧 English
Afsluitmodus
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
LED-helderheid
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)
Slaapstand
i
Controls whether the device enters low-power sleep when idle.
Normal (sleep when idle)
Batterijmonitor
i
Monitors battery voltage during the flight.
DISABLED
Cloud group
i
The cloud group / category this flight is assigned to.
General use
GP6 / GP7 poorten
GP-poortbesturing was niet beschikbaar voor firmware 2.0
I2C PCA9685 Servoboard
GP-poortbesturing was niet beschikbaar voor firmware 2.0
Voorspelling en luchtremmen
Deze functie was niet beschikbaar voor versie 2.10+
Reacties
Reacties
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