Main Links
- Current release on GitHub
- Getting Started
- Pictures
- Breadboard
- Assembly and Components
- Fly Test
- Bootup Configuration File
- Project Progress Page
- Free DIY Resources
Reference Configuration
Since it is possible to change some characteristic of the unit selecting different hardware, we propose a reference configuration. The reference configuration will have the following characteristics (complete hardware). This unit can determine True Airspeed, Mach number, Altitude, and common air properties from a pitot-static probe data and an outside air temperature probe.
Overall weight: 47 grams
Overall dimensions: Without push in fittings 66x41x24 mm; With push-in fittings 81x41x24 mm. Fixing tabs dimensions are equal to those of a standard servo
Assembly time: About 1.5 hours
Overall cost: 160 Eur (June 2017)
Power and Supply Current: Power to the ADC is supplied through a standard micro USB port, the same can be used to transfer data. The typical power source is a cell phone power bank
Ratings: Maximum measurable IAS @ standard conditions and . /382.06 km/h. /120.82 km/h. Raw sensor Range (-1,+1) Psi. Sample speed 50 Hz (user selectable). Altitude, ISA (<4000, ) MSL. Raw sensor Range (0, 160000) Pa. Sample speed 50 Hz (user selectable). Uncertainty , 0.056 m @ 50 MSL and 0.064 m @ 1000 MSL
Bluetooth: Present, usable with a custom library to interact with an Android phone
Micro SD Card Reader: Present, micro SD Card 4GB
Temperature measurement: Present, uncalibrated typical 2 deg accuracy
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