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.
Errors compound across frames, sensors, estimators, dynamics, control laws, timing, and actuators.
Vectors, Euler angles, DCMs, quaternions, and interpolation define orientation consistently.
IMU, magnetometer, barometer, calibration, noise, bias, and timing define what can be observed.
Complementary and Kalman-family filters turn measurements into attitude, velocity, position, and uncertainty.
Rigid-body motion, rotor forces, torque, actuator lag, gravity, and integration define the plant.
PID, LQR, MPC, robust control, mixing, constraints, and saturation turn state error into commands.
Zephyr targets, telemetry, simulation, rigs, and thrust measurement close the loop with hardware.
The diagram separates demonstrated mathematics and software from in-progress and planned work. It is a maturity map, not a finished-product claim.
These repositories are public for inspection. Check each repository for its own reuse terms.
Quaternion, Euler, DCM, vector, and SLERP mathematics.
Complementary filters, EKF, bias, magnetometer, and altitude fusion.
Six-DOF rigid-body motion, linearization, rotor thrust, torque, and induced velocity.
PID, LQR, MPC, H-infinity, mixers, and closed-loop simulation.
Estimator, controller, dynamics, and hardware abstraction integration.
Visualization, tuning, telemetry, and physical propulsion measurement.
Roadmap language is not presented as measured capability.
Core math, models, estimators, controllers, embedded experiments, and rigs are publicly inspectable.
The work is converging toward consistent simulation, hardware-in-the-loop, and controlled physical tests.
Higher-level autonomy follows reliable estimation, control, timing, and safety evidence.
The current work is engineering research, not a certified flight-control product.