Projection-free computation of robust controllable sets with constrained zonotopes
Abraham P. Vinod, Avishai Weiss, Stefano Di Cairano
TL;DR
The paper tackles robust controllable set computation for discrete-time linear systems with additive uncertainty by introducing a projection-free, least-squares framework based on constrained zonotopes. It develops both inner and outer approximations of Pontryagin differences where the minuend is a CZ and the subtrahend is symmetric, convex, and compact, with closed-form results for several common subtrahends (ellipsoids, zonotopes, and their unions). These approximations feed into efficient RC-set recursions, yielding scalable inner RC sets for high-dimensional problems and enabling exactness under invertible CZ representations. The approach is validated through case studies including a 100D RC set and abort-safe spacecraft rendezvous, demonstrating orders-of-magnitude speedups over traditional polytope-based methods while maintaining meaningful accuracy. Overall, the work provides a practical, scalable solution for robust planning and verification in high-dimensional systems with structured uncertainties.
Abstract
We study the problem of computing robust controllable sets for discrete-time linear systems with additive uncertainty. We propose a tractable and scalable approach to inner- and outer-approximate robust controllable sets using constrained zonotopes, when the additive uncertainty set is a symmetric, convex, and compact set. Our least-squares-based approach uses novel closed-form approximations of the Pontryagin difference between a constrained zonotopic minuend and a symmetric, convex, and compact subtrahend. Unlike existing approaches, our approach does not rely on convex optimization solvers, and is projection-free for ellipsoidal and zonotopic uncertainty sets. We also propose a least-squares-based approach to compute a convex, polyhedral outer-approximation to constrained zonotopes, and characterize sufficient conditions under which all these approximations are exact. We demonstrate the computational efficiency and scalability of our approach in several case studies, including the design of abort-safe rendezvous trajectories for a spacecraft in near-rectilinear halo orbit under uncertainty. Our approach can inner-approximate a 20-step robust controllable set for a 100-dimensional linear system in under 15 seconds on a standard computer.
