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System Overview

The OnSpeed Gen3 is a self-contained AOA computer built around an ESP32-S3 microcontroller. Here's what's inside and how the pieces fit together.

What's in the Box

The Gen3 controller board includes:

Component Part Function
Microcontroller ESP32-S3-WROOM-2 (32MB flash, 8MB PSRAM) Runs everything — AHRS, audio, WiFi, logging
IMU IMU330 (accel + gyro) Measures pitch, roll, and accelerations at 416 Hz
Pitot Pressure Honeywell HSCMRRN001PDSA3 Dynamic pressure for airspeed (14-bit SPI)
AOA Pressure Honeywell HSCMRRN001PDSA3 Differential pressure from AOA probe (14-bit SPI)
Static Pressure Honeywell HSCMRNN1.6BASA3 Barometric pressure for altitude/density
Audio DAC I2S output Stereo audio at 16 kHz sample rate
SD Card microSD slot Flight data logging at 50 Hz
WiFi Built into ESP32-S3 Web-based configuration and log download
External ADC MCP3202 (12-bit, V4P hardware) Reads flap position potentiometer and volume knob
Voltage Regulator L7805ABD2T-TR Accepts 12–28V aircraft power, provides 5V

System Block Diagram

graph TD
    subgraph Aircraft
        PP[Pitot Port] --> PS1[Pitot Sensor]
        AP[AOA Probe] --> PS2[AOA Sensor]
        SP[Static Port] --> PS3[Static Sensor]
        EFIS[EFIS Serial Out] --> |"115200 baud"| EI[EFIS Input]
        PWR[12-28V Aircraft Power] --> VREG[5V Regulator]
    end

    subgraph OnSpeed Controller
        PS1 --> SPI[SPI Bus]
        PS2 --> SPI
        PS3 --> SPI
        IMU[IMU330] --> SPI
        SPI --> ESP[ESP32-S3]
        EI --> ESP
        VREG --> ESP
        ESP --> I2S[I2S Audio Out]
        ESP --> SD[microSD Card]
        ESP --> WIFI[WiFi AP]
        ESP --> LED[Status LED]
        ESP --> |optional| DISP[External Display]
    end

    I2S --> |Headset/Panel| AUDIO[Audio Panel or Headset]
    WIFI --> |192.168.0.1| BROWSER[Web Browser]

    style ESP fill:#2196F3,color:#fff
    style AUDIO fill:#4CAF50,color:#fff

Data Flow

Every 20 milliseconds (50 Hz), the system:

  1. Reads pressure sensors — pitot, AOA, and static pressures via SPI
  2. Reads the IMU — accelerometer and gyroscope at 416 Hz (the pressure sensors read at 50 Hz)
  3. Runs the AHRS algorithm — EKFQ (default) or Madgwick fuses IMU data into pitch/roll/heading
  4. Computes Derived AOA — SmoothedPitch - FlightPath (where FlightPath = arcsin(VSI / TAS))
  5. Calculates IAS — from pitot dynamic pressure
  6. Reads EFIS data — if connected, gets IAS, pitch, OAT, altitude from your glass panel
  7. Detects flap position — from potentiometer or jumper settings
  8. Selects tone — maps AOA against the current flap setting's thresholds
  9. Generates audio — I2S stereo output with optional 3D panning
  10. Logs to SD card — all sensor data, computed values, and state

Connections to Your Aircraft

The controller needs the following connections:

Required

  • 12–28V power — from aircraft bus through a circuit breaker
  • Pitot line — connects to your pitot system (tee fitting)
  • AOA line — connects to your AOA pressure probe
  • Static line — connects to your static system (tee fitting)
  • Audio output — to audio panel or headset (see Audio Wiring)
  • EFIS serial — from your Dynon, Garmin, or MGL for IAS, OAT, and attitude data
  • Flap position — potentiometer or jumper wires for flap detection

Optional

  • OAT sensor (DS18B20) — if you don't have an EFIS providing outside air temperature
  • External display — M5Stack or similar for cockpit display
  • Boom probe — reference AOA probe for testing/calibration

Software Architecture

The firmware runs as a set of FreeRTOS tasks on the ESP32-S3's dual cores:

Core Tasks Priority
Core 1 (flight-critical) Sensors, IMU, Audio, Display Serial, Flaps, G-limit, Volume, Vno Chime, 3D Audio High
Core 0 (connectivity) WiFi, Web Server, WebSocket Data Server, Log Writer, Heartbeat LED Lower

This separation ensures that sensor reading and audio generation are never blocked by WiFi traffic or web page serving.

AHRS Algorithms

OnSpeed supports two attitude estimation algorithms, selectable in configuration:

  • EKFQ (default) — 11-state quaternion Extended Kalman Filter. Estimates attitude, gyro biases, vertical velocity and altitude, vertical-accel bias, and sideslip. Optuna-tuned against a VectorNav VN-300 reference.
  • Madgwick — Complementary filter using quaternion math. Lower CPU cost.

Switching algorithms requires recalibration

The calibration wizard fits AOA curves against Derived AOA, which differs between Madgwick and EKFQ. If you change your AHRS algorithm, you must re-fly the calibration wizard.