Build autonomous flight from equations that survive contact with hardware.

The programme connects attitude mathematics, noisy sensors, state estimation, rigid-body dynamics, control, embedded execution, and physical test rigs.

Each layer is developed as an inspectable contract before it becomes an autonomy claim.

FLIGHT CONTROL · FROM EQUATIONS TO HARDWARE
Build autonomous flight from equations that survive contact with hardware. engineering system

Flight control is a chain of models, not one PID loop

Errors compound across frames, sensors, estimators, dynamics, control laws, timing, and actuators.

THE EXECUTION PATH

Frames + attitude

Vectors, Euler angles, DCMs, quaternions, and interpolation define orientation consistently.

01

Sensors

IMU, magnetometer, barometer, calibration, noise, bias, and timing define what can be observed.

02

State estimation

Complementary and Kalman-family filters turn measurements into attitude, velocity, position, and uncertainty.

03

Vehicle dynamics

Rigid-body motion, rotor forces, torque, actuator lag, gravity, and integration define the plant.

04

Control

PID, LQR, MPC, robust control, mixing, constraints, and saturation turn state error into commands.

05

Embedded + validation

Zephyr targets, telemetry, simulation, rigs, and thrust measurement close the loop with hardware.

06

Autonomy matures one verified contract at a time

The diagram separates demonstrated mathematics and software from in-progress and planned work. It is a maturity map, not a finished-product claim.

AUTONOMOUS SYSTEMS
Autonomy maturity chain covering perception, state and navigation, energy and endurance, safety and verification, field sensing, and remote deployment.

The mathematical stack is split into inspectable systems

These repositories are public for inspection. Check each repository for its own reuse terms.

PUBLIC ENGINEERING RECORD

attitudeMathLibrary

Quaternion, Euler, DCM, vector, and SLERP mathematics.

ATTITUDE

stateEstimation

Complementary filters, EKF, bias, magnetometer, and altitude fusion.

ESTIMATION

dynamic_models + rotorDynamics

Six-DOF rigid-body motion, linearization, rotor thrust, torque, and induced velocity.

DYNAMICS

controlSystems

PID, LQR, MPC, H-infinity, mixers, and closed-loop simulation.

CONTROL

inertial_navigation_system

Estimator, controller, dynamics, and hardware abstraction integration.

INTEGRATION

AeroDynControlRig + ThrustStand

Visualization, tuning, telemetry, and physical propulsion measurement.

TEST SYSTEMS

What exists now, and what remains work

Roadmap language is not presented as measured capability.

EVIDENCE BEFORE CLAIMS

Mathematics and software components

Core math, models, estimators, controllers, embedded experiments, and rigs are publicly inspectable.

DEMONSTRATED

Integrated validation

The work is converging toward consistent simulation, hardware-in-the-loop, and controlled physical tests.

IN PROGRESS

Autonomous systems

Higher-level autonomy follows reliable estimation, control, timing, and safety evidence.

PLANNED

Production flight certification

The current work is engineering research, not a certified flight-control product.

NOT CLAIMED