calculate /systems/pitot/total-pressure on the bases of /velocities/mach
authorEric van den Berg <evan_den_berg@hotmail.com>
Mon, 26 Nov 2012 17:59:48 +0000 (18:59 +0100)
committerJames Turner <zakalawe@mac.com>
Mon, 28 Jan 2013 16:54:35 +0000 (16:54 +0000)
commit5a8e6aeb8626db27fc606da1e0c8dfa913c88265
treec19bfaae6c5f4e235e75a17188a8d3a3d3828657
parent5826cea0a832864d0c61fced20288f687578d4b1
calculate /systems/pitot/total-pressure on the bases of /velocities/mach
added measured-total-pressure property to account for a normal
shockwave in front of pitot tube at supersonic speeds. momentarily not
used
small unit conversion correction of inHg to hPa in altimeter
Base airspeed calculations on impact pressure in instrumentation
/airspeed_indicator
src/Instrumentation/airspeed_indicator.cxx
src/Instrumentation/airspeed_indicator.hxx
src/Instrumentation/altimeter.cxx
src/Systems/pitot.cxx
src/Systems/pitot.hxx