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Drag-Aware Aerodynamic Manipulability for Torque-Limited Redundant Multirotors: Aerodynamic Promptness based on the Symmetric Acceleration Capacity

arXiv 2603.07998 ↗First posted 9 Mar 2026cs.RO cs.AI cs.SYcited by 0

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Abstract (arXiv)

Aerodynamic promptness quantifies how rotor-speed variations generate multirotor wrench variations, but its Euclidean formulation assigns the same local cost to a given rotor acceleration at every operating speed. This work develops a capacity-aware extension for redundant multirotors with arbitrary numbers of heterogeneous rotors and wrench components. Under bounded motor torque and aerodynamic drag, each generally asymmetric instantaneous rotor-acceleration interval contains a largest zero-centered subset whose radius defines the symmetric acceleration capacity (SAC). The SAC induces a Riemannian metric on the positive-capacity rotor-speed region. Propagating its co-metric through the nonlinear rotor-speed-to-wrench differential yields a state-attached task-rate capability matrix and ellipsoid. The corresponding inverse quadratic form equals the minimum normalized rotor-acceleration effort required to realize a prescribed wrench rate, while the ellipsoid volume defines the drag-aware aerodynamic manipulability (DAAM) index. Fiberwise DAAM maximization provides a task-coordinate-invariant criterion for selecting task-equivalent actuator states; its maximizing set exists on compact regular domains and can be nonconvex and set valued. Low-dimensional two- and three-rotor studies make the resulting fiberwise geometry and parameter dependence directly visible. A complementary two-rotor use case shows how DAAM can inform a continuous allocation section subject to directional motor-torque feasibility. For two heterogeneous propulsion systems, the resulting sections reduce saturation-induced force-tracking degradation relative to the pseudoinverse in the faster command bands

Key facts. No citing papers in the map yet (data through 14 Oct 2026). Builds on 6 of its 32 references that are in the map. First posted on arXiv 9 Mar 2026.

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References · 6

  1. 2021A Comparative Study of Nonlinear MPC and Differential-Flatness-Based Control for Quadrotor Agile Flightcited by 24
  2. 2021Time-Optimal Planning for Quadrotor Waypoint Flightcited by 23
  3. 2021Performance, Precision, and Payloads: Adaptive Nonlinear MPC for Quadrotorscited by 18
  4. 2022Downwash-aware Control Allocation for Over-actuated UAV Platformscited by 3
  5. 2022Feasible Wrench Set Computation for Legged Robotscited by 1
  6. 2026Muscle Coactivation in the Sky: Geometry and Pareto Optimality of Energy vs. Aerodynamic Promptness and Multirotors as Variable Stiffness Actuatorscited by 1

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