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Battery-Swapping Multi-Agent System for Sustained Operation of Large Planetary Fleets

Ethan Holand, Jarrod Homer, Alex Storrer, Musheeera Khandeker, Ethan F. Muhlon, Maulik Patel, Ben-oni Vainqueur, David Antaki, Naomi Cooke, Chloe Wilson, Bahram Shafai, Nathaniel Hanson, Taşkın Padır

TL;DR

This work proposes a battery-swapping, hub-mediated power architecture to sustain fleets of small planetary rovers, reducing rover SWAP-C by outsourcing generation to a central hub and swapping in fully charged modules for near-continuous operation. It presents a low-cost, open-source test platform and a docking/swapping protocol validated through autonomous docking, swapping, and field testing, achieving an average service time of $98$ seconds and expanding the robust docking configuration space by $258\%$ through design optimization. The approach leverages a generalized hub-rover architecture with a formal capacity equation $n_r=\left\lfloor\frac{P_{gen}-P_h}{\max(Q_bV_b/C, P_m)}\right\rfloor$, enabling scalable fleets and potential extensions for communications and computation at the hub. While demonstrated on Earth as a proof of concept, the work discusses environmental, thermal, and radiation considerations and outlines future steps toward space readiness and more extensive trade studies on power transfer modalities and cost-benefit analyses.

Abstract

We propose a novel, heterogeneous multi-agent architecture that miniaturizes rovers by outsourcing power generation to a central hub. By delegating power generation and distribution functions to this hub, the size, weight, power, and cost (SWAP-C) per rover are reduced, enabling efficient fleet scaling. As these rovers conduct mission tasks around the terrain, the hub charges an array of replacement battery modules. When a rover requires charging, it returns to the hub to initiate an autonomous docking sequence and exits with a fully charged battery. This confers an advantage over direct charging methods, such as wireless or wired charging, by replenishing a rover in minutes as opposed to hours, increasing net rover uptime. This work shares an open-source platform developed to demonstrate battery swapping on unknown field terrain. We detail our design methodologies utilized for increasing system reliability, with a focus on optimization, robust mechanical design, and verification. Optimization of the system is discussed, including the design of passive guide rails through simulation-based optimization methods which increase the valid docking configuration space by 258%. The full system was evaluated during integrated testing, where an average servicing time of 98 seconds was achieved on surfaces with a gradient up to 10°. We conclude by briefly proposing flight considerations for advancing the system toward a space-ready design. In sum, this prototype represents a proof of concept for autonomous docking and battery transfer on field terrain, advancing its Technology Readiness Level (TRL) from 1 to 3.

Battery-Swapping Multi-Agent System for Sustained Operation of Large Planetary Fleets

TL;DR

This work proposes a battery-swapping, hub-mediated power architecture to sustain fleets of small planetary rovers, reducing rover SWAP-C by outsourcing generation to a central hub and swapping in fully charged modules for near-continuous operation. It presents a low-cost, open-source test platform and a docking/swapping protocol validated through autonomous docking, swapping, and field testing, achieving an average service time of seconds and expanding the robust docking configuration space by through design optimization. The approach leverages a generalized hub-rover architecture with a formal capacity equation , enabling scalable fleets and potential extensions for communications and computation at the hub. While demonstrated on Earth as a proof of concept, the work discusses environmental, thermal, and radiation considerations and outlines future steps toward space readiness and more extensive trade studies on power transfer modalities and cost-benefit analyses.

Abstract

We propose a novel, heterogeneous multi-agent architecture that miniaturizes rovers by outsourcing power generation to a central hub. By delegating power generation and distribution functions to this hub, the size, weight, power, and cost (SWAP-C) per rover are reduced, enabling efficient fleet scaling. As these rovers conduct mission tasks around the terrain, the hub charges an array of replacement battery modules. When a rover requires charging, it returns to the hub to initiate an autonomous docking sequence and exits with a fully charged battery. This confers an advantage over direct charging methods, such as wireless or wired charging, by replenishing a rover in minutes as opposed to hours, increasing net rover uptime. This work shares an open-source platform developed to demonstrate battery swapping on unknown field terrain. We detail our design methodologies utilized for increasing system reliability, with a focus on optimization, robust mechanical design, and verification. Optimization of the system is discussed, including the design of passive guide rails through simulation-based optimization methods which increase the valid docking configuration space by 258%. The full system was evaluated during integrated testing, where an average servicing time of 98 seconds was achieved on surfaces with a gradient up to 10°. We conclude by briefly proposing flight considerations for advancing the system toward a space-ready design. In sum, this prototype represents a proof of concept for autonomous docking and battery transfer on field terrain, advancing its Technology Readiness Level (TRL) from 1 to 3.
Paper Structure (31 sections, 9 equations, 12 figures, 3 tables)

This paper contains 31 sections, 9 equations, 12 figures, 3 tables.

Figures (12)

  • Figure 1: Field Testing of the prototype battery-swapping multi-agent rover architecture. The large rover, left, generates and distributes power to an internal cache of battery modules. The small rover, right, docks with the base to hot-swap its spent battery for one with full charge.
  • Figure 2: Battery swapping method represented schematically.
  • Figure 3: Final prototype with labeled components.
  • Figure 4: Step-by-step process diagram of docking and battery swap procedure. After step D, the procedure is reversed to complete a swap.
  • Figure 5: Block diagram representing critical electrical components for power transfer across a hub, battery module, and rover.
  • ...and 7 more figures