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The flight simulation is available on the cal/test tab of the FIP.  Follow the on-screen 
directions and button labels to perform the flight.  You can control the duration of the 5G 
acceleration, even turning it on and off to simulate multiple-stage flights or air-starts.  
The Raven records all the data just as if it were a real flight, so you can familiarize 
yourself with the Raven operation and data review. 
 
The simulated flight assumes that the Apo output channel is used for apogee deployment, 
and the Main output channel is used for main deployment.   When the apogee channel 
fires, the simulation applies a 100 ft/second descent rate.  When the main output fires, a 
descent rate of 20 feet/second is applied.  The other two outputs have no effect on the 
simulated flight trajectory. 
 
Although the Raven can be mounted in your rocket with either end up, the simulated 
flight must be conducted with the screw terminal block up.  This is because the simulated 
thrust is implemented as a test mode of the accelerometer chip that applies the 
acceleration in a single direction, only  
 

Caution:  Do not run a flight simulation with e-matches or igniters connected unless 
the igniters/e-matches are located away from flammable materials and adequate 
ventilation is provided.  In particular, do not run a flight simulation with black powder 
charges or motors connected! 

Viewing the data 

A data file from a previous download 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 the plot using the 
Parameter selection tool bar.  Multiple measurements can be plotted on the same time 
scale by holding down the <control> key when selecting the traces. 
 
The lower section of the parameter selection toolbar allows you to select flight event 
logic that was recorded during the flight.  The flight event logic states are the conditions 
that are measured by the Raven and used in the deployment control logic.  The 
deployment output fires when all of the checked logic conditions are true.  By plotting the 
voltage on each of the outputs and the flight event logic that was checked during the 
flight, you can verify exactly what the altimeter was firing, when, and why.  This is 
useful for verifying a flight program by looking at the data recorded in a simulated flight, 
which records data just as a real flight would. 
 
To zoom in on a particular range of time, drag with the left mouse button just underneath 
the time axis.   Click the right mouse button to zoom out or type in the axis ranges.  To 
zoom in on the vertical axis for a measurement, drag with the left mouse button on the 
measurement axis you want to change. 
 
To export formatted data into a separate analysis tool (such as Matlab or a spreadsheet), 
right-click in the parameter selection window, which brings up options for saving as a 
delimited file or copying data to the clipboard, where it can be pasted directly into a 
spreadsheet. 
 

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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