doc: Add asciidoc version of altosui chapter.

Signed-off-by: Keith Packard <keithp@keithp.com>

1 files changed, 5 insertions, 111 deletions

diff --git a/doc/system-operation.inc b/doc/system-operation.inc
index 1e57f247..bca1ee80 100644
--- a/doc/system-operation.inc
+++ b/doc/system-operation.inc
@@ -1,3 +1,4 @@
+[appendix]
 == System Operation
 
 	=== Firmware Modes
@@ -34,7 +35,7 @@
 		long). “Brap” means a long dissonant tone.
 
 		.AltOS Modes
-		[options="border",cols="1,1,1,1"]
+		[options="border",cols="1,1,2,2"]
 		|====
 		|Mode Name
 		|Abbreviation
@@ -127,7 +128,7 @@
 		Here's a summary of all of the “pad” and “idle” mode indications.
 
 		.Pad/Idle Indications
-		[options="header",cols="1,1,1"]
+		[options="header",cols="1,1,3"]
 		|====
 		|Name		|Beeps		|Description
 
@@ -619,112 +620,5 @@
 			to activate the channel. The conditions
 			available are:
 
-			Acceleration:: Select a value, and then choose
-			whether acceleration should be above or below
-			that value. Acceleration is positive upwards,
-			so accelerating towards the ground would
-			produce negative numbers. Acceleration during
-			descent is noisy and inaccurate, so be careful
-			when using it during these phases of the
-			flight.
-
-			Vertical speed:: Select a value, and then
-			choose whether vertical speed should be above
-			or below that value. Speed is positive
-			upwards, so moving towards the ground would
-			produce negative numbers. Speed during descent
-			is a bit noisy and so be careful when using it
-			during these phases of the flight.
-
-			Height:: Select a value, and then choose
-			whether the height above the launch pad should
-			be above or below that value.
-
-			Orientation:: TeleMega and EasyMega contain a
-			3-axis gyroscope and accelerometer which is
-			used to measure the current angle. Note that
-			this angle is not the change in angle from the
-			launch pad, but rather absolute relative to
-			gravity; the 3-axis accelerometer is used to
-			compute the angle of the rocket on the launch
-			pad and initialize the system.
-
-			  [NOTE]
-			  ====
-			  Because this value is computed by integrating
-			  rate gyros, it gets progressively less
-			  accurate as the flight goes on. It should have
-			  an accumulated error of less than 0.2°/second
-			  (after 10 seconds of flight, the error should
-			  be less than 2°).
-
-			  The usual use of the orientation configuration
-			  is to ensure that the rocket is traveling
-			  mostly upwards when deciding whether to ignite
-			  air starts or additional stages. For that,
-			  choose a reasonable maximum angle (like 20°)
-			  and set the motor igniter to require an angle
-			  of less than that value.
-			  ====
-
-			Flight Time:: Time since boost was
-			detected. Select a value and choose whether to
-			activate the pyro channel before or after that
-			amount of time.
-
-			Ascending:: A simple test saying whether the
-			rocket is going up or not. This is exactly
-			equivalent to testing whether the speed is
-			> 0.
-
-			Descending:: A simple test saying whether the
-			rocket is going down or not. This is exactly
-			equivalent to testing whether the speed is
-			< 0.
-
-			After Motor:: The flight software counts each
-			time the rocket starts accelerating and then
-			decelerating (presumably due to a motor or
-			motors burning). Use this value for
-			multi-staged or multi-airstart launches.
-
-			Delay:: This value doesn't perform any checks,
-			instead it inserts a delay between the time
-			when the other parameters become true and when
-			the pyro channel is activated.
-
-			Flight State:: The flight software tracks the flight
-			through a sequence of states:
-
-			 * Boost. The motor has lit and the rocket is
-			   accelerating upwards.
-
-			 * Fast. The motor has burned out and the
-			   rocket is decelerating, but it is going
-			   faster than 200m/s.
-
-			 * Coast. The rocket is still moving upwards
-			   and decelerating, but the speed is less
-			   than 200m/s.
-
-			 * Drogue. The rocket has reached apogee and
-			   is heading back down, but is above the
-			   configured Main altitude.
-
-			 * Main. The rocket is still descending, and
-			   is below the Main altitude
-
-			 * Landed. The rocket is no longer moving.
-
-			You can select a state to limit when the pyro
-			channel may activate; note that the check is
-			based on when the rocket transitions *into*
-			the state, and so checking for “greater than
-			Boost” means that the rocket is currently in
-			boost or some later state.
-
-			When a motor burns out, the rocket enters
-			either Fast or Coast state (depending on how
-			fast it is moving). If the computer detects
-			upwards acceleration again, it will move back
-			to Boost state.
+			include::pyro-channels.raw[]
+