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Open-source purpose-built robots

How heavy must a purpose-built UAV for targeted observation be, and when does a hover-capable airframe stop being worth its weight?

research/osrobot-uav

How heavy must a purpose-built UAV for targeted observation be, and when is a hover-capable airframe worth its weight? At 3 km out and 20 min on station a fixed wing closes at 1.27 kg against 2.14 kg for a quadrotor and 2.08 kg for a VTOL wing, and the quadrotor stops closing at 45 min (stylised, assumed constants, no flight stack run).

8 tests

What it found

A stdlib mass-closure sizing model closes a quadrotor, a fixed wing and a fixed wing with a vertical-lift system for the same mission, choosing rotor diameter or wing area for least mass. For 3 km out, 20 min on station and a 0.5 kg payload the plain fixed wing is lightest (1.27 kg), against 2.14 kg for the quadrotor and 2.08 kg for the VTOL wing. The quadrotor does not close at 45 min on station; the VTOL wing is lighter than it from 30 min or beyond about 10 km. Stylised: every technology constant is assumed, no flight stack was run, and a fixed wing cannot hover or launch unaided.

A figure from its own output

Figure produced by research/osrobot-uav: mass_sweeps
osrobot-uav/experiments/mass_sweeps.svg, written by the project's own experiment code.

Paper, code and results

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Produced with AI assistance (Claude). Results are from the code in this repository and are simulated or stylised unless the abstract says otherwise; nothing here implies affiliation with or endorsement by any lab, researcher or company cited. MIT licensed.