@@ -25,3 +25,27 @@ g1 --> Ascent
```
# Avionics Design
```mermaid
%%{init: {'theme':'neutral'}}%%
flowchart LR;
t[Teensy 4.1]
imu[Inertial Measurement Unit]
b[Barometer]
subgraph Propulsion
r[Roll Motor]
p[Pitch Motor]
end
imu & b -. I2C .-> t
t -- PWM --> r & p
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