STM32 Flight Controller

A KiCad hardware project for an STM32-based flight controller with inertial, barometric and optional navigation sensing.

A KiCad hardware project for an STM32F4-class UAV flight controller with inertial, barometric and optional navigation sensing.

In development

01Project brief

Scope and current stage.

This page reports the documented state of the work. It does not represent qualification, manufacturing release, or operational deployment unless stated explicitly.

Objective: Establish a configurable controller platform for UAV experimentation, with firmware integration explicitly left as future work.
Development stage: Hardware design · firmware pending
Technology areas: STM32F4KiCadUAV
Publication note: Further specifications are withheld until they are supported by the current engineering record.

02Notes

Background

Small UAV platforms benefit from a configurable controller base that can be re-flashed, re-tasked and re-pinned without re-spinning the board. This project defines such a base and explicitly defers firmware integration to a later stage.

03Engineering record

Documented architecture

Compute

MCU: STM32F4 class
Tooling: KiCad schematic + PCB

Sensing

IMU: Inertial interface
Barometer: Pressure interface
Navigation: Optional external interface

Stage

Hardware: Design package
Firmware: Pending — out of current scope

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