Patent · US Active

Control system for automatic circle flight

US8078395B2 · kind B2 · utility

17Cited by
10References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 15, 2005
Grant dateDec 13, 2011
Priority date
Expiry dateJul 7, 2028

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG05D1/0202
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

A flight control system for an aircraft is configured for receiving command signals representing commanded values of a location of a geospatial point and a radius about the geospatial point for defining a circular groundtrack. A sensor determines a geospatial location of the aircraft and provides a location signal representing the location of the aircraft. A controller for commanding flight control devices on the aircraft controls the flight of the aircraft and is configured to receive the command signals and the location signal. The controller uses the command signals and location signal to operate the flight control devices to control the flight of the aircraft for directing the aircraft generally toward a tangent point of the circular groundtrack and then maintaining a flight path along the circular groundtrack.

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