Patent · US Active

Simultaneously cost-optimized and policy-compliant trajectory generation for unmanned aircraft

US11262746B1 · kind B1 · utility

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25Claims
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Key dates

Filing dateJun 17, 2019
Grant dateMar 1, 2022
Priority date
Expiry dateMar 13, 2040

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG08G5/59
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

A flight processor that calculates a 4-dimensional trajectory having a sequence of two or more position, time and cost (x, y, z, t, c) tuples that minimize a defined cost. Some embodiments generate cost-optimized trajectories with simple or complex constraints and bounds such as fixed AGL altitude; minimum AGL altitude; maximum AGL altitude; minimum MSL; maximum MSL; avoidance of restricted airspace; adherence to non-restricted airspace such as easements; adherence to ground-based guideways, if applicable; and the constraint to maintain adequate radio frequency signal-to-noise needed for communications to the ground station or backhaul systems. Constraint-enabled minimization of trajectory cost may leverage the aircraft's energy model; current atmospheric data (most notably wind vector data along the trajectory path); continuous-time and/or event-based risk models and fault trees; blacklisted and white-listed geo-fence boundaries; defined easements; and known or estimated RF signal-to-noise (SNR) minimum values needed for one or two-way communications.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.