Patent · US Active

Flight modes and protection envelopes based on inertial attitude estimates for radio-controlled airplanes

US9753457B2 · kind B2 · utility

1Cited by
1References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 11, 2015
Grant dateSep 5, 2017
Priority date
Expiry dateMay 11, 2035

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64U2201/20
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

The present disclosure describes flight training systems and methods for radio-controlled (RC) airplanes that rely on inertial attitude estimates. Preferred embodiments include an RC airplane with one or more control processors configured to (i) estimate an inertial attitude of the RC airplane based on one or more measurements from an attitude sensor array and (ii) control the inertial attitude of the RC airplane based the inertial attitude estimate. In operation, controlling the attitude of the RC airplane may include both controlling the RC airplane to a specific inertial attitude and/or keeping the inertial attitude of the RC airplane within a predefined flight envelope.

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