The N-5 Scaling Law: Topological Dimensionality Reduction in the Optimal Design of Fully-actuated Multirotors
Antonio Franchi

TL;DR
This paper uncovers the topological structure of optimal rotor configurations in fully-actuated multirotors, revealing a phase transition and a predictable N-5 scaling law that enables continuous reconfiguration while maintaining optimal control.
Contribution
It introduces a topological analysis of the design landscape, discovering a phase transition and the N-5 Scaling Law that characterize optimal configurations for various multirotor geometries.
Findings
Optimal configurations form discrete points or continuous curves depending on chassis regularity.
The N-5 Scaling Law predicts the number of topological branches for N <= 10.
Reconfiguration along these branches preserves optimal isotropic control authority.
Abstract
The geometric design of fully-actuated and omnidirectional N-rotor aerial vehicles is conventionally formulated as a parametric optimization problem, seeking a single optimal set of N orientations within a fixed architectural family. This work departs from that paradigm to investigate the intrinsic topological structure of the optimization landscape itself. We formulate the design problem on the product manifold of Projective Lines \RP^2^N, fixing the rotor positions to the vertices of polyhedral chassis while varying their lines of action. By minimizing a coordinate-invariant Log-Volume isotropy metric, we reveal that the topology of the global optima is governed strictly by the symmetry of the chassis. For generic (irregular) vertex arrangements, the solutions appear as a discrete set of isolated points. However, as the chassis geometry approaches regularity, the solution space…
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