Bob, sorry for the misunderstanding. By ~1g I meant 1 gram for the arming switch, not 1 gravity. The arming switch I'm referring to is
this simple screw switch. The Parrot's liftoff detection algorithm looks for a delta-V of about 6 mph, which equates to a pretty good intentional shake. Tilting it up or down or even dropping it a few inches on the launch rail won't cause a false trigger.
I agree that someone could make their own 2-cell, Li-Po battery to use with the AA-1 to make the masses comparable. The user would also have to either get a single-cell Li-po charger and charge the cells individually, or a 2-cell charger and manage the cell balancing. For the Parrot, the USB connection does the charging, and includes limits on charging current and voltage, in addition to the cell's own independent cell protection circuitry that covers overcharge, overdischarge, and over-current faults.
Here is some more comparison information:
Advantages for the AA-1:
-1000 Hz accel sampling, vs. the Parrot's 200 Hz. From the data I've seen, this isn't very important for integrating the velocity, but it would provide significantly better data for looking at the details of the deployment dynamics.
-Custom interface software. Probably easier to use than the Parrot's method of capturing the data using Hyperterminal and then pasting into an Excel template.
-Blinks out the estimated altitude. With the Parrot, you have to use the Excel template before you know how high it went.
-Options for higher-range accelerometers. I think the Parrot uses the same accelerometer parts, but I didn't think to include some +/- 120 or +/- 250 G versions in the initial production run.
-More options for the deployment trigger. Can do it a configurable time after launch, burnout, or apogee.
-Audible continuity indication
Advantages for the Parrot:
-Barometric altimeter. Enables descent rate measurement and is used together with the accel for the best estimate of Cd. (explanation of why the baro would be useful for Cd calculation available on request)
-Lateral acceleration. Can be useful for estimating the rocket spin rate, getting visibility into deployment/landing dynamics, launch guide issues, or other times something goes wrong. I used data from it to determine that an unstable flight in one of my rockets was due primarily to CG/thrust misalignment rather than pure aerodynamic instability.
-Lighter, when using the manufacturer-recommended battery (9V).
-Measures and records temperature, battery voltage, and sensor reference voltage. These are mostly just for curiosity, except:
-All measurements have built-in temperature compensation, based on end-to-end calibrations at two different temperatures, and the in-flight temperature measurements. Without it, a 40 degree F temperature difference would cause about 1.5% (accel) to 3% (baro) errors in the sensor scale factors for the Parrot. I don't know how senstive the end-to-end system of the AA-1 is to temperaure, though I think it uses the same accelerometer.
-Records 5 flights, rather than 1. Useful if you don't want to bring a laptop out to the range.
-Records 5:08 of high-rate data, plus 25 minutes of low-rate data, compared to 33 seconds for the AA-1 (at its highest data rate). This isn't a key discriminator, except that it points out that without barometric data, there isn't really much to record after a few seconds after burnout.
-USB connection to the PC, rather than RS-232.
Everyone, feel free to let me know if I have any errors in the above.
Reading over this thread, I would be surprised if you didn't need more than 70 Gs for the accel range. I may be able to swap out the 70g accel on an already-built board to take advantage of all the other machine-placed parts. The accels in the higher ranges are only single-axis, but they have the same footprint as the 70/35 2-axis one I use, and they just don't use the extra pad. The rework would be tricky, but I'll take a closer look to see if I think I could do it.