12.07.2015 Views

SkyView System Installation Guide - Dynon Avionics

SkyView System Installation Guide - Dynon Avionics

SkyView System Installation Guide - Dynon Avionics

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

SV-ADAHRS-20X <strong>Installation</strong> and ConfigurationPerforming Pitot-Static ChecksBackground<strong>Dynon</strong> ADAHRS units use airspeed in the calculation of attitude (or GPS ground speed whenairspeed is unavailable). The internal rate sensors are monitored and calibrated in flight usingfeedback from the accelerometers and from airspeed to achieve a highly accurate attitudesolution.When a pitot or static test is performed the ADAHRS is being exposed to dynamics that areimpossible to achieve in a real aircraft flight environment, namely, large airspeed changeswithout the accompanying accelerations and rotations. This false condition will cause a wellcalibratedunit to incorrectly adjust its calibration. Furthermore, when a unit is in a testsituation a change in applied pitot or static pressure will cause the attitude to pitch up or down.This is expected.Performing the following <strong>Dynon</strong>-prescribed pitot and static test procedure to a <strong>Dynon</strong> ADAHRSwill prevent problems with the unit’s performance in flight.Pitot/Static Test InstructionsBasic PrinciplesStepsEnsure <strong>SkyView</strong> is warmed up during each test reading.<strong>SkyView</strong> should be powered off when changing pressures.Keep aircraft still (do not move) when pressure is applied.1. The aircraft itself should be temperature stable. For example, if the aircraft is movedfrom outside in the sun to a hangar for testing, tests should not be started until theairplane has stabilized at the hangar temperature.2. Turn <strong>SkyView</strong> on and let it warm up until the altitude reading is stabilized. This periodshould be at least 5 minutes, but may take longer depending on environmentalconditions.3. Turn <strong>SkyView</strong> off.4. While <strong>SkyView</strong> is off, apply the pressure required by your test to pitot and/or static portvia your test equipment.5. Turn on <strong>SkyView</strong> (external or internal battery power is acceptable). Keep aircraft stillwhile <strong>SkyView</strong> is powered on. Do not adjust the pitot or static pressures being applied tothe ADAHRS while it is powered on.6. Verify airspeed and/or altitude reading.7. Turn <strong>SkyView</strong> off (using button 1 is a good option for this operation).8. Repeat steps 4-7 for each required pressure point in the test.5-10 <strong>SkyView</strong> <strong>System</strong> <strong>Installation</strong> <strong>Guide</strong> - Revision O

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!