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added ignitor and battery to avionics

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Anson Biggs
2021-04-01 00:15:31 +00:00
parent 6aa3879ee3
commit ab56095ac7
1 changed files with 4 additions and 1 deletions
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readme.md
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@@ -33,6 +33,7 @@ g1 --> Ascent
%%{init: {'theme':'neutral'}}%% %%{init: {'theme':'neutral'}}%%
flowchart LR; flowchart LR;
batt[Battery]
t[Teensy 4.1] t[Teensy 4.1]
imu[Inertial Measurement Unit] imu[Inertial Measurement Unit]
b[Barometer] b[Barometer]
@@ -40,12 +41,14 @@ b[Barometer]
subgraph Propulsion subgraph Propulsion
r[Roll Motor] r[Roll Motor]
p[Pitch Motor] p[Pitch Motor]
e[Engine Ignitor]
end end
imu & b -. I2C .-> t imu & b -. I2C .-> t
batt == 3.3V ==> t
t -- PWM --> r & p t -- PWM --> r & p & e
``` ```