diff options
author | Keith Packard <keithp@keithp.com> | 2015-11-13 20:58:58 -0800 |
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committer | Keith Packard <keithp@keithp.com> | 2015-11-13 20:58:58 -0800 |
commit | 6260ee1419ba5c122939b28e3e8fc6f8ecf48928 (patch) | |
tree | 829ab59192d0ffbd5e737966e4d238193dac6c9e /doc/usage.inc | |
parent | 2133c235af9511a42b65b239c6fcbeafa0e6d272 (diff) |
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>
Diffstat (limited to 'doc/usage.inc')
-rw-r--r-- | doc/usage.inc | 78 |
1 files changed, 78 insertions, 0 deletions
diff --git a/doc/usage.inc b/doc/usage.inc index b2ab0c27..caccc168 100644 --- a/doc/usage.inc +++ b/doc/usage.inc @@ -124,6 +124,84 @@ |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 |