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Startseite
Gerät: N-P85-E090
Flug-ID: 639
Flugzusammenfassung
Höhe
Apogäum
76.72 Meter
Zeit bis Apogäum
4.4 seconds
Brennschluss-Höhe
38.95 m
Max. Geschw.-Höhe
13.55 m
Auswurf-Höhe
70.13 m
Lande-Höhe
-1.7 m
Stabilität
Stabilitätswert
49.8 / 100 (Ausreichend)
Stabilitätsaufschlüsselung
Neigung bei Brennschluss (20%)22.4
Neigungskonstanz (15%)71.1
Nick/Gier-Rate (30%)16.6
Dämpfung (20%)81.7
Schubgeradheit (15%)88.6
Geschwindigkeit
Max. Aufstieg
41.23 m/s
Max. Abstieg
-18.32 m/s
Bei Brennschluss
22.300 m/s
Landegeschw.
-12.347 m/s
Abstiegsgeschw.
-9.031 m/s
Auswurfgeschw.
1.30 m/s
Recovery
Single deploy (no dual deploy detected)
Beschleunigung
Max. Aufstieg
6.17 G
Max. Abstieg
2.48 G
Max. während Brennen
6.17 G
Durchschn. Aufstieg
0.2 G
Durchschn. Brennen
2.64 G
Zeiten
Brennschluss (erster)
1.3 seconds
Apogäum
4.4 seconds
Möglicher Auswurf
5.201 seconds
Landung
12.23 seconds
Ausgang #1 EIN
0 seconds
Ausgang #1 AUS
0 seconds
Winkel
Rampen-Neigung
3.00°
Max. Neigung bis Brennschluss
16.88°
Start-Roll
-2.89°
Start-Nick
-0.78°
Max. Drehung (Brennen)
1592.03 dps
Durchschn. Drehung (Brennen)
877.79 dps
Allgemein
Upload-Datum
02-Nov at 18:07
Datenpunkte
857
Gesamte Aufnahmezeit
26.800 s
Durchschn. Abtastrate/s
31.9
Anzahl Sperren
1
Aufnahme-Höhe
110.29 m
Start nach Einschalten
15m 17s
Referenzachse
X
Batterie & Temperatur
Batterie Start
0%
Batterie Ende
0%
Temperatur Start
16.34°C
Temperatur Ende
16.39°C
MT1 Starttemp.
0°C
Ausgangsregeln
Keine Regeln konfiguriert
Flugdaten-Animation
FLIGHT 639
76.72 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
Hinweis: Die Fluganimation erfordert eine feste Ausrichtung Ihres Höhenmessers. Kalibrieren Sie Ihre Sensoren für beste Ergebnisse.
Benutzernotizen
Fügen Sie dieses Gerät Ihrem Konto hinzu, um zu bearbeiten
Youtube-Video
Kein Video
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Flugbilder (0)
Keine Bilder
Verknüpfte Rakete
Keine Rakete mit diesem Flug verknüpft
Geräteinformationen
Mercury V1
Dieser Flug wurde mit einem geflogen: Mercury V1.
Hardwareversion
Rev 1
Softwareversion
1.3
Zuletzt online
02-Nov at 18:12
Beschleunigungssensor
32G 3-axis
Gyroskop
2000 dgps 3-axis
Drucksensor
Bosch BMP 390
Magnetometer
N/A
Flugmotoren
Keine Motoren zu diesem Flug hinzugefügt
Fügen Sie dieses Gerät Ihrem Konto hinzu, um zu bearbeiten
Startplatz, Datum & Uhrzeit
Klicken Sie auf die Karte, um Ihren Startplatz zu markieren. Wechseln Sie zwischen Karten- und Satellitenansicht.
No results found — try a different search.
Klicken Sie auf die Karte · Ziehen zum Anpassen
Lat—
Lng—
✓ Launch location saved successfully.
✗ Could not save location — please try again.
Ausgangsregeln
Ausgangsregeln were not available until firmware 2.0
Motor-Zuordnung (BETA)
Noch im Testmodus! Wir arbeiten daran, den passenden Motor für einen Flug zu ermitteln.
Marke
Motor
Punkte
Form
Brennen
Estes
1/4A3T
115
95%
82.9%
Cesaroni
25-E75-VM-17A
65
92.1%
93.7%
AeroTech
I1299N
63
91.1%
92.8%
Cesaroni
68-F240-VM-15A
60
94.3%
94.1%
AeroTech
H669N
53
94.9%
94.1%
Estes
1/2A6
29
92.7%
73.7%
Contrail
G300
13
57.5%
70.5%
Estes
1/2A3T
11
87.7%
90%
AeroTech
G339N
0
50.5%
90.4%
Motorbrenndauer
Dies ist die Beschleunigungssensor-Gesamtgröße vom Start bis Brennschluss.
You can check this against your motors thrust data on thrustcurve.org.
Allgemeine Flugeinstellungen
Dies ist ein Schnappschuss der für diesen Flug verwendeten Einstellungen. Gehen Sie zur
Gehen Sie zur Meine Geräte Seite und konfigurieren Sie die Einstellungen..
Prognosedruck
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 mbar
Starterkennung
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
Abtastrate
i
The base sample rate of the altimeter's sensors in samples per second. This setting was deprecated in firmware 2.0+.
32 Hz
Abtastverhältnis
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:
Max. Abtastungen
i
This is the maximum samples the altimeter will log per flight. When it reaches this amount it will stop and save the recording.
0
Aufnahme-Stopp
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.
4x 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 3
Druckfilter
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)
Sperrzeit
i
The Lockout time is how long the altimeter should stop making decisions and taking actions if it detects unusual high speed altitude changes that are unexpected.
These false readings can be caused by ejection charges (if the altimeter is in the same compartment as the motor ejection gases) or even when you transition to Mach speeds and can give false readings of altitude changes.
When these events are detected the system enters Lockout for the specified time while it stabalises. This effects things like triggering the output, or calculating other data.
These false readings can be caused by ejection charges (if the altimeter is in the same compartment as the motor ejection gases) or even when you transition to Mach speeds and can give false readings of altitude changes.
When these events are detected the system enters Lockout for the specified time while it stabalises. This effects things like triggering the output, or calculating other data.
750ms
Sperränderung
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.
1.5 meters
Sensorsynchronisation
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.
AKTIVIERT (10 samples / 312.00ms)
Ausrichtung
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
Start-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.
1.4G
Startsperre
i
When enabled, the altimeter locks out recording for a set period after power on to prevent false triggering during setup.
DISABLED
Statische Temperatur
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.
Ausgangseinstellungen
Dies ist ein Schnappschuss der für diesen Flug verwendeten Einstellungen.
Ausgang 1 aktiviert
i
Disable or enable the output from being able to turn on or off.
DEAKTIVIERT
Ausgang 1 Auslöser
i
After apogee (altitude)
This method triggers when the altitude drops below the set altitude after apogee is detected.After apogee (time)
This method triggers the defined seconds after apogee is detected.After launch (altitude)
This method is activated if/once the altimeter exceeds the set altitude after launch.After launch (time)
This option triggers the defined seconds after launch is detected.After burnout (time)
This method triggers the defined seconds after burnout is detected.
After apogee (altitude)
Ausgang 1 Einschaltzeit
i
This is how long the output should trigger ON state when the rules are met.
2000ms
Ausgang 1 Höhe
i
This is the altitude to trigger at if using a trigger method that works on altitude.
For example if you set this to 75m and After apogee (altitude) for the trigger then the output will turn on at 75m on descent above the launch altitude.
For example if you set this to 75m and After apogee (altitude) for the trigger then the output will turn on at 75m on descent above the launch altitude.
0 meters
Ausgang 1 Zeit
i
This is the time variable for output triggers that work on time.
For example if you set this to 3 seconds and After apogee (time) as the trigger then the output will turn on 3 seconds after apogee.
For example if you set this to 3 seconds and After apogee (time) as the trigger then the output will turn on 3 seconds after apogee.
0 seconds
Höhensperre
i
Altitude lock is a safety feature that prevents the output from triggering if the altitude is below this level when the rules are met.
50.00 m
Neigungssperre
i
This is another safety feature. It can be used to disable the output if the rocket has gone too far from vertical.
For example if you set the tilt angle lock to 40 degrees then the output will not fire if the rocket is more than 40 degrees from vertical. To disable set this to 0.
For example if you set the tilt angle lock to 40 degrees then the output will not fire if the rocket is more than 40 degrees from vertical. To disable set this to 0.
0.00 °
Sensorkalibrierung
Kalibrierungsversätze für diesen Flug.
Gyroskop
⚠ Gyroskop wurde nicht kalibriert
X
0.000°
Y
0.000°
Z
0.000°
Beschleunigungssensor
⚠ Beschleunigungssensor wurde nicht kalibriert
X
0.000 mG
Y
0.000 mG
Z
0.000 mG
Geräteeinstellungen
Dies ist ein Schnappschuss der für diesen Flug verwendeten Einstellungen.
Dies ist ein Schnappschuss der für diesen Flug verwendeten Einstellungen.
Geräte-TAG
i
A custom name or tag assigned to this device for easy identification.
Merc8853
Sprache
i
The language setting configured on the device.
en
Abschaltmodus
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-Helligkeit
i
The brightness level of the LED indicators on the Mercury. Lower values save battery.
WLAN-Sendeleistung
i
WiFi transmit power level. Higher gives better range but uses more battery.
Schlafmodus
i
Controls whether the device enters low-power sleep when idle.
Stay awake
Batterieüberwachung
i
Monitors battery voltage during the flight.
ENABLED
Cloud-Gruppe
i
The cloud group / category this flight is assigned to.
GP6 / GP7 Anschlüsse
GP-Portsteuerung war erst ab Firmware 2.0 verfügbar
I2C PCA9685 Servoplatine
GP-Portsteuerung war erst ab Firmware 2.0 verfügbar
Vorhersage und Luftbremsen
Diese Funktion war erst ab Version 2.10+ verfügbar
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