Multicopter attitude control for recovery from large disturbances

Abstract

We present a novel, high-performance attitude control law for multicopters, with a view to recovery from large disturbances. The controller is compared to three well-established alternatives from the literature. All controllers considered are identical to first order, but differ in their computation of the attitude error. We show that the popular use of the skewsymmetric part of the rotation matrix is problematic from a safety perspective, and specifically that the closed loop system may linger at large attitude errors for an arbitrary duration (leading to potential failures of practical systems). The novel proposed controller prioritizes the error in the vehicle thrust direction, and is shown to outperform a similar, existing controller from the literature. Stability follows via a Lyapunov function, and the controller is validated in experiments. This novel controller is especially attractive in safety-critical situations, where a multicopter may be required to recover from large initial disturbances.

A flow disturbance estimation and rejection strategy for multirotors with round-trip trajectories

“…Both controllers were performed offboard, while the total torque is calculated onboard. A nonlinear controller, which prioritizes yaw angle being matched with the desired yaw angle [19] is used in attitude control.…”