Failover navigation for remotely operated aerial vehicles
US10394240B1 · kind B1 · utility
Assignee
Inventor
Key dates
| Filing date | Apr 27, 2017 |
| Grant date | Aug 27, 2019 |
| Priority date | — |
| Expiry date | Jul 7, 2037 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64U2201/20
- WIPO fieldControl
- WIPO sectorInstruments
Abstract
The present invention extends to methods, systems, devices, and apparatus for failover navigation for remotely operated aerial vehicles. During flight, a primary guidance system uses a higher resolution map for an area to guide a remotely operated aerial vehicle around obstacles (e.g., buildings) in the area. Failure of the primary guidance system is detected during flight. The remotely operated aerial vehicle switches over to a secondary guidance system in response to detecting the failure. The secondary guidance system formulates a flight path to a safer location based on a lower resolution map of the area. The formulated flight path minimizes crossings between different boundaries represented in the lower resolution map. The formulated flight path is biased towards safety over efficiency.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.