Patent · US Active

Control system for vehicles

US8014909B2 · kind B2 · utility

18Cited by
5References
24Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 25, 2004
Grant dateSep 6, 2011
Priority date
Expiry dateOct 26, 2026

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64U2201/10
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A system for controlling flight of an aircraft has sensors (37, 43), a receiver (45), and a digital control system (57), all of which are carried aboard the aircraft. The sensors (37, 43) determine the position of the aircraft relative to the earth and the inertial movement of the aircraft. The receiver (45) receives transmitted data (51, 55) communicating the position and movement of a reference vehicle relative to the earth. The control system (57) calculates the position and velocity of the aircraft relative to the reference vehicle using the data from the sensors (37, 43) and the receiver (45) and then commands flight control devices (33) on the aircraft for maneuvering the aircraft in a manner that maintains a selected position and/or velocity relative to the reference vehicle. The system allows use of a graphical or tactile user interfaces.

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