X-Git-Url: https://git.gag.com/?p=fw%2Faltos;a=blobdiff_plain;f=doc%2Faltusmetrum.xsl;h=39b3998a5154f35e35fa9042b56222b79340e736;hp=d3d1f72a9e1228e9536c9610a4a9a9f4387f6e7f;hb=0bf1c74e83fe49a11916b52596363f4dd56c522c;hpb=874d0065ecb066ee746a016876edebc7cc6e3d96 diff --git a/doc/altusmetrum.xsl b/doc/altusmetrum.xsl index d3d1f72a..39b3998a 100644 --- a/doc/altusmetrum.xsl +++ b/doc/altusmetrum.xsl @@ -1539,10 +1539,13 @@ NAR #88757, TRA #12200 first five seconds of operation. - At power on, you will hear three beeps or see three flashes - (“S” in Morse code for start up) and then a pause while - the altimeter completes initialization and self test, and decides - which mode to enter next. + At power on, the altimeter will beep out the battery voltage + to the nearest tenth of a volt. Each digit is represented by + a sequence of short “dit” beeps, with a pause between + digits. A zero digit is represented with one long “dah” + beep. Then there will be a short pause while the altimeter + completes initialization and self test, and decides which mode + to enter next. Here's a short summary of all of the modes and the beeping (or @@ -1570,7 +1573,7 @@ NAR #88757, TRA #12200 Startup S - dit dit dit + battery voltage in decivolts Calibrating sensors, detecting orientation. @@ -2180,6 +2183,20 @@ NAR #88757, TRA #12200 way quite happily, including Keith's successful L3 cert. +
+ Apogee Lockout + + Apogee lockout is the number of seconds after boost where + the flight computer will not fire the apogee charge, even if + the rocket appears to be at apogee. This is often called + 'Mach Delay', as it is intended to prevent a flight computer + from unintentionally firing apogee charges due to the pressure + spike that occurrs across a mach transition. Altus Metrum + flight computers include a Kalman filter which is not fooled + by this sharp pressure increase, and so this setting should + be left at the default value of zero to disable it. + +
Main Deployment Altitude