Pioneer Rocketry Flight Computer

Pioneer Rocketry’s latest generation flight computer for high power, STM32-based avionics system designed for experimental high-power rockets. It provides state estimation, real-time telemetry, staging logic, and fully active control capabilities. This repository contains the firmware, test tools, and documentation for the system.

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Prerequisites

Before building this project, ensure you have the following tools installed and added to your system PATH:

1. Visual Studio Code or STM32CubeIDE
2. STM32CubeMX (v6.13 or newer) - Required to generate hardware config.
3. Make Use winget install ezwinports.make or choco install make - Build system generator.
4. Arm GNU Toolchain - The compiler (e.g., arm-none-eabi-gcc).
5. Ninja Build (Optional) - A faster build system than Make.

VS Code Extensions

Install the following extensions within VS Code:

• Cortex Debug

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Build Instructions

1. Clone and Open

Clone the repository and open the folder in VS Code:

git clone --recurse-submodules https://github.com/Pioneer-Rocketry/Flight-Computer.git

2. Build the Firmware

You can build the project using the status bar at the bottom or the Command Palette:

• Status Bar: Click Build (or the generic "Gear" icon).
• Shortcut: Press F7.

Successful build output will create a Code.elf and Code.bin file in the ./Code/build/ directory.

3. Flash and Debug

Connect your STM32 board via ST-Link.

1. Press F5 to start debugging.
2. The extension will automatically:

• Build the latest code.
• Flash the board using OpenOCD/ST-Link.
• Open the debug console.

Troubleshooting

• "Multiple target patterns" error: Ensure your project folder path contains NO SPACES (e.g., use C:\Dev\Project instead of C:\Users\My Name\Project).
• C++ vs C: If main.cpp is not being compiled, check CMakeLists.txt to ensure CXX is enabled and main.cpp is listed in the source files. If main.c is in the CDEF, remove it and delete the file.

Hardware Overview

Primary Components

Function	Component
Main MCU	STM32F446RE
High-G IMU (Accel + Gyro)	LSM6DSV32X
Magnetometer	MMC5603
Barometer	MS5607-02BA03
GPS	u-blox SAM-M8Q
Radio	LoRa SX1262

Additional Hardware Features

• 3 independent pyrotechnic deployment channels
• Breakouts for I²C and SPI expansion
• Support for 4 servo channels (vectoring, control surfaces, etc.)
• USB/Serial connectivity for configuration and simulation
• Ruggedized PCB designed for high-G, high-speed flight

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Software Overview

The firmware is written in modern C++, using HAL for low-level drivers and a modular class-based architecture for sensors, telemetry, and estimation modules.

Key Capabilities

• State estimation for:
  • Attitude (roll, pitch, yaw)
  • Position (x, y, z)
  • Velocity and angular rates (Uses a custom multi-sensor Kalman Filter.)
• Live telemetry over LoRa
• Event-driven flight logic, including:
  • Ascent/descent detection
  • Apogee detection
  • Staging and separation logic
  • Deployment sequencing
• Active Control
  • Servo-driven stabilization or thrust-vectoring
  • Optional closed-loop controls for advanced tests
• Fault-tolerant design
  • Sensor redundancy
  • Fail-safe deployment rules
  • Logging of all states and events

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Testing Strategy

Hardware-in-the-Loop Testing (HILT)

HILT allows the flight computer to run full flight software using simulated sensor data.

• The board connects to a PC via USB/Serial.
• A custom simulator streams “fake” IMU, barometer, and GPS data.
• The firmware behaves exactly as if it were in flight.
• Allows testing:
  • Sensor fusion
  • State transitions
  • Staging logic
  • Deployment logic
  • Data logging and telemetry

This framework accelerates development and eliminates many failure modes before field testing.

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Field & Flight Testing

Flight testing follows a staged, risk-managed approach:

1. Initial flights: Validate basic state estimation (position, velocity, attitude) and state transitions.
2. Intermediate flights: Add automated apogee deployment, then drogue/main testing, then multistage events.
3. Advanced flights:
   • High-speed, high-G tests
   • Full staging logic
   • Active control (servo-active fins or TVC)
   • Redundancy and fault recovery tests

Each successful flight unlocks the next feature set, ensuring safe and repeatable progress toward fully active control.

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Repository Structure

Flight-Computer/
├── Code/
│   ├── Core/
│   │   ├──Src/
│   │   └── Inc/
│   └── lib/
├── Datasheets/
└── PCB/