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Accel calibrations used during the flight 

 

Pad altitude ASL 

After the first few minutes of flight, the data recording changes to a lower rate, and stores 
approximately 35 minutes more.  The liftoff mode will continue, and deployment outputs 
will function if necessary, after the end of the data recording.  The liftoff mode only ends 
when landing is detected. 
When the flight conditions assigned for each output are true, 

(See configuring the Raven 

using the FIP section)

 the output switch will turn on.  The default deployment conditions 

are the following: 
 

Output function 

Apogee 

deployment 

Main chute 

deployment 

Backup apogee 

deployment 

Backup Main 

deployment 

Altimeter output 
Label 

Apo 

Main 

3

rd

 

4th 

Upward velocity 
(from accel) 

< 400 ft/sec 

< 400 ft/sec 

< 0 ft/sec 

< 400 ft/sec 

Baro altitude 

Decreasing 

Decreasing 

Increasing or 

decreasing 

Decreasing 

Altitude above pad 

Any 

< 700 feet 

Any 

< 700 feet 

Time delay 

2 sec 

1.5 sec 

Burnout Counter 

 
These default output settings can easily be changed using the Featherweight Interface 
Program (FIP). 

Post-flight operation 

When the Raven is below 2000 feet above the launch pad, it watches 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 
battery life. 
To hear the peak altitude after recovery, pick up the rocket or av-bay and tilt it one 
direction and then another.  When the Raven detects that it has been flipped over, it will 
beep out the altitude again.   The Raven will beep out each decimal of a 5 decimal 
altitude, in feet, starting with the 10,000 place.  A pause between sets of beeps indicates a 
change to the next decimal place.  A short, low beep indicates a 0 in that decimal place.  
For example, 1024 feet is represented as <low beep, for zero in the 10,000 place>, pause, 
<one high beep> pause <one low beep> pause <2 high beeps> pause <4 high beeps>. 
The button can be used to switch between post-landing mode and wait mode.  Whenever 
the mode is switched into wait mode, the last apogee altitude will be repeated. 

Computer-Attached Operations 

Featherweight Interface Program (FIP) Installation: 

Download the FIP installation package from the Featherweight site.  The installation 
package contains both the FIP and the USB drivers necessary for the Raven to interface 
with the computer.  Double-click on the zip package and follow the installation package 
instructions. 

Содержание Raven3

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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