AltusMetrum Setup Guide
Full manual: The Altus Metrum System: An Owner’s Manual for Altus Metrum Rocketry Electronics
RF Link
To interact with the telmega you will need to use the TeleBT to connect over rf link. There is also a way to do it directly through micro-usb but for some reason this never works. Connect the teleBT to a laptop and launch AltOS. If it can’t find the teleBT as a device, the battery is probably just very dead and it might need to charge for a little while.
When using the RF link it is important to know which mode the flight computer is in. The Telemetrum and Telemega have two starup modes: Idle and Pad.
Idle Mode
The computer enters this mode if it is powered on while turned sideways. When in this mode the computer is only receiving signals so you can use Configure Altimeter
, Save Flight Data
, Monitor Idle
, and Fire Igniter
. While in this mode the board will only beep on startup. To connect to the computer you will need to use the correct channel and callsign. If you don't know what channel or callsign the computer is set to, you can find out by powering it on in Flight Mode, then using Scan Channels
. The ground station callsign can be changed in Configure Altos UI
, and the channel can be changed in Configure Ground Station
. The factory default should be using channel 0 (434.550 Mhz) and callsign N0CALL.
Configure Altimeter
Can change callsign and channel from here, along with other settings.
Use the Reboot
button on the Configure Flight Computer
menu to restart the board. If the orientation is correct this can allow switching from Idle to Pad mode from a distance.
Extra Event Pyro Configuration
For triggering pyros for other events, such as staging.
Pad Mode
The computer enters this mode if it is powered on while pointing up. When in this mode the computer will only transmit signals, not receive them. While is this mode you can use Scan Channels
to find the right computer and Monitor Flight
to view the data. While in the mode the board will beep frequently (a series of beeps over five seconds).
Beeping
In the description of the beeping pattern, “dit” means a short beep while "dah" means a long beep (three times as long). “Brap” means a long dissonant tone.
Mode Indicator Beeps
Mode Name | Abbreviation | Beeps | Description |
Startup | S | battery voltage in decivolts | Calibrating sensors, detecting orientation. |
Idle | I | dit dit | Ready to accept commands over USB or radio link. |
Pad | P | dit dah dah dit | Waiting for launch. Not listening for commands. |
Boost | B | dah dit dit dit | Accelerating upwards. |
Fast | F | dit dit dah dit | Decelerating, but moving faster than 200m/s. |
Coast | C | dah dit dah dit | Decelerating, moving slower than 200m/s |
Drogue | D | dah dit dit | Descending after apogee. Above main height. |
Main | M | dah dah | Descending. Below main height. |
Landed | L | dit dah dit dit | Stable altitude for at least ten seconds. |
Sensor error | X | dah dit dit dah | 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.
Idle and Pad Mode Beeps
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. |
Additional Igniters | four very short beeps | Continuity indication for the additional pyro channels on TeleMega, EasyMega and EasyTimer. One high tone for no continuity, one low tone for continuity. On TeleMega and EasyMegay, these are produced after the continuity indicators for the two primary igniter channels. |