Koopman Operator Based Modeling and Control of Rigid Body Motion Represented by Dual Quaternions

TL;DR

This paper develops a finite-dimensional Koopman operator-based linear model for rigid body dynamics using dual quaternions, enabling effective control design with LQR and demonstrating promising simulation results.

Contribution

The paper introduces a systematic method to derive finite observables for Koopman modeling of rigid body dynamics with dual quaternions, ensuring accurate approximation and control.

Findings

Finite set of Koopman observables converges pointwise to zero.

Lifted linear model enables LQR control of rigid body.

Control performance comparable to nonlinear controllers.

Abstract

In this paper, we systematically derive a finite set of Koopman based observables to construct a lifted linear state space model that describes the rigid body dynamics based on the dual quaternion representation. In general, the Koopman operator is a linear infinite dimensional operator, which means that the derived linear state space model of the rigid body dynamics will be infinite-dimensional, which is not suitable for modeling and control design purposes. Recently, finite approximations of the operator computed by means of methods like the Extended Dynamic Mode Decomposition (EDMD) have shown promising results for different classes of problems. However, without using an appropriate set of observables in the EDMD approach, there can be no guarantees that the computed approximation of the nonlinear dynamics is sufficiently accurate. The major challenge in using the Koopman operator for constructing a linear state space model is the choice of observables. State-of-the-art methods in the field compute the approximations of the observables by using neural networks, standard radial basis functions (RBFs), polynomials or heuristic approximations of these functions. However, these observables might not providea sufficiently accurate approximation or representation of the dynamics. In contrast, we first show the pointwise convergence of the derived observable functions to zero, thereby allowing us to choose a finite set of these observables. Next, we use the derived observables in EDMD to compute the lifted linear state and input matrices for the rigid body dynamics. Finally, we show that an LQR type (linear) controller, which is designed based on the truncated linear state space model, can steer the rigid body to a desired state while its performance is commensurate with that of a nonlinear controller. The efficacy of our approach is demonstrated through numerical simulations.