doc: Move pad beeps table to usage chapter

This places all of the sound information in one place.

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

diff --git a/doc/system-operation.inc b/doc/system-operation.inc
index dd8d7d02041793e6b913a7553702034574edcce6..4503f525e0f9c495ec8da7c96b482299c7079601 100644 (file)
--- a/doc/system-operation.inc
+++ b/doc/system-operation.inc
@@ -59,39 +59,8 @@
                memory, the flight computer will emit a warbling tone (much
                slower than the “no continuity tone”)
 
                memory, the flight computer will emit a warbling tone (much
                slower than the “no continuity tone”)
 

-               Here's a summary of all of the “pad” and “idle” mode indications.
-
-               .Pad/Idle Indications
-               [options="header",cols="1,1,3"]
-               |====
-               |Name           |Beeps          |Description
-
-               |Neither
-               |brap
-               |No continuity detected on either apogee or main igniters.
-
-               |Apogee
-               |dit
-               |Continuity detected only on apogee igniter.
-
-               |Main
-               |dit dit
-               |Continuity detected only on main igniter.
-
-
-               |Both
-               |dit dit dit
-               |Continuity detected on both igniters.
-
-
-               |Storage Full
-               |warble
-               |On-board data logging storage is full. This will
-                not prevent the flight computer from safely
-                controlling the flight or transmitting telemetry
-                signals, but no record of the flight will be
-                stored in on-board flash.
-               |====
+               See <<_understanding_beeps>> for a summary of all of
+               the audio signals used.

 
                Once landed, the flight computer will signal that by emitting
                the “Landed” sound described above, after which it will beep
 
                Once landed, the flight computer will signal that by emitting
                the “Landed” sound described above, after which it will beep

diff --git a/doc/usage.inc b/doc/usage.inc
index b2ab0c2700dfcc7e89629079825a4c46b18daa94..caccc168bd3bdbce4f04b0f0a73ad62f336121c5 100644 (file)
--- a/doc/usage.inc
+++ b/doc/usage.inc
@@ -124,6 +124,84 @@
                |Error detected during sensor calibration.
                |====
 
                |Error detected during sensor calibration.
                |====
 

+               Here's a summary of all of the Pad and Idle mode
+               indications. In Idle mode, you'll hear one of these
+               just once after the two short dits indicating idle
+               mode. In Pad mode, after the dit dah dah dit
+               indicating Pad mode, you'll hear these once every five
+               seconds.
+
+               .Pad/Idle Indications
+               [options="header",cols="1,1,3"]
+               |====
+               |Name           |Beeps          |Description
+
+               |Neither
+               |brap
+               |No continuity detected on either apogee or main igniters.
+
+               |Apogee
+               |dit
+               |Continuity detected only on apogee igniter.
+
+               |Main
+               |dit dit
+               |Continuity detected only on main igniter.
+
+
+               |Both
+               |dit dit dit
+               |Continuity detected on both igniters.
+
+
+               |Storage Full
+               |warble
+               |On-board data logging storage is full. This will
+                not prevent the flight computer from safely
+                controlling the flight or transmitting telemetry
+                signals, but no record of the flight will be
+                stored in on-board flash.
+               |====
+
+               For devices with a radio transmitter, in addition to
+               the digital and APRS telemetry signals, you can also
+               receive audio tones with a standard amateur
+               70cm FM receiver. While on the pad, you will hear
+               igniter status once every five seconds.
+
+               .Pad Radio Indications
+               [options="header",cols="1,1,3"]
+               |====
+               |Name           |Beeps          |Description
+
+               |Neither
+               |½ second tone
+               |No continuity detected on either apogee or main igniters.
+
+               |Apogee
+               |dit
+               |Continuity detected only on apogee igniter.
+
+               |Main
+               |dit dit
+               |Continuity detected only on main igniter.
+
+
+               |Both
+               |dit dit dit
+               |Continuity detected on both igniters.
+
+               |====
+
+               During ascent, the tones will be muted to allow the
+               telemetry data to consume the full radio bandwidth.
+
+               During descent and after landing, a ½ second tone will
+               be transmitted every five seconds. This can be used to
+               find the rocket using RDF techniques when the signal
+               is too weak to receive GPS information via telemetry
+               or APRS.
+

        === Turning On the Power
 
                Connect a battery and power switch and turn the switch
        === Turning On the Power
 
                Connect a battery and power switch and turn the switch