background image

Calibration and Accuracy: 

The barometric sensor used in the Raven is a digital-output sensor that contains the entire 
analog measurement chain on one chip.  The sensor is factory-calibrated over a wide 
range of temperatures and pressures to provide exceptional accuracy under any rocketry 
conditions.  The combination of individual chip calibration and end-to-end temperature 
compensation provides barometric accuracy that raises the bar for rocketry altimeters.  
The Raven has less than 1 mbar (0.1% full-scale) pressure error over most conditions, 
and less than 3 mbar pressure error (0.3%) the temperature range from -40C to 85C, and 
from 1.1 Atm (2500 feet below sea level) to 0.3 Atm (30,000 feet above sea level). 
 
Keep in mind that however accurately the Raven measures pressure, converting pressure 
to altitude results in additional error.  The Raven uses the International Standard 
Atmosphere (ISA) model, which uses 3 different formulas for different altitude ranges 
between sea level and 104,987 feet to compensate for the temperature behavior of 
different parts of the atmosphere.  The standard atmosphere model is implemented in the 
Raven with full ANSI-C floating point calculations to avoid errors from numerical 
approximations.  The standard atmosphere model, however, is an approximation to 
typical conditions for mid-latitude locations.  It assumes a temperature profile that is 
likely to be colder than typical rocketry conditions.  For example, the standard 
atmosphere model assumes that the sea-level temperature is 59 F, and that the 
temperature at 5400 feet ASL is 40F.  Errors caused by the atmosphere being warmer 
than the standard atmosphere can result in reported altitudes that are low by 10% or more.  
For the most accurate conversion between the pressure and altitude, use the twice-daily 
balloon sounding data measured by NOAA and conveniently available at 

http://weather.uwyo.edu/upperair/sounding.html

.  Future versions of the FIP may include 

an option for automated lookup and correction based on this data. 

Specifications: 

Contact Information: 

Email:  

[email protected]

  

Brand 

Featherweight 

Model 

Raven3 

Axial Accel range and 

frequency 

105Gs, 400Hz 

Axial Accel resolution 

0.045 Gs 

Lateral Accel range and 

frequency 

105 Gs, 200 Hz 

Lateral Accel Resolution 

0.09 Gs 

Download Interface 

USB mini 

Baro Range (kft) 

100 

Baro resolution 

0.00004 atm 

Pyro Outputs 

Single-battery max output 

Amps 

22 

2-battery max output Amps 

22 

Other recorded 

measurements 

Temperature, 4 

continuity voltages, 

all event logic, 

battery V 

High-rate recording time 

480 seconds 

Low-rate recording time 

35 minutes 

Size 

0.8" x 1.8" x 0.5"  

Mass 

6.6 grams 

Summary of Contents for Raven3

Page 1: ...ff Detection and flight 4 Post flight operation 5 Computer Attached Operations 5 Featherweight Interface Program FIP Installation 5 Connecting to the Raven using the FIP 6 Raven Status and Data Downlo...

Page 2: ...description of the default program for the 4 outputs is given in the deployment programming section of this document Caution Do not use this or any other altimeter for deployments until you have perf...

Page 3: ...mers love the Featherweight screw switch because of its reliability tiny size and convenient mounting terminals The screw head wipes and preloads the contacts with every operation The Featherweight ma...

Page 4: ...rocket is dropped a short distance the Raven will ignore the subsequent contact to avoid premature liftoff detection Despite these features it is possible for the Raven to misinterpret normal handling...

Page 5: ...atches for the barometric readings to become constant to detect landing After landing the altitude at apogee will be beeped out once and then the red LED will flash once per second These features save...

Page 6: ...altimeter model and the comm port to which the Raven is connected If multiple comm ports show up in the dialog box the highest numbered one will probably be the one with the Raven connected to it The...

Page 7: ...ommand Configuring the Raven using the FIP To program and verify the deployment options programmed into your Raven click the Configure tab The logic used for each deployment output is represented as a...

Page 8: ...ty 0 feet second used for the backup apogee deployment channel This trigger is true when the upward velocity has stopped and the rocket is starting to fall The Raven senses the acceleration and subtra...

Page 9: ...ser timer value and Time user timer value This condition is true when the elapsed time from liftoff detection is less than or greater than the user settable timer threshold TVal TVal can be set from 0...

Page 10: ...e adding 1 to the burnout count When the burnout counter is greater than or equal to the user burnout count for that output channel the trigger will be true Unlike the burnout counter used in other al...

Page 11: ...nload can be opened for viewing using the File Open command The default set of measurements shows the altitude above the pad in feet and the axial accelerometer trace Additional traces can be added to...

Page 12: ...oximations The standard atmosphere model however is an approximation to typical conditions for mid latitude locations It assumes a temperature profile that is likely to be colder than typical rocketry...

Reviews: