Correction of vibration-induced error for touch screen display in an aircraft
US10996793B2 · kind B2 · utility
Assignee
Inventors
Key dates
| Filing date | Jun 20, 2017 |
| Grant date | May 4, 2021 |
| Priority date | — |
| Expiry date | Aug 31, 2037 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB60K2360/199
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
Systems and methods for correcting a vibration-induced error on a touch screen display device on an aircraft are provided. A method can include providing a user interface for display on a touch screen display device. The user interface can include one or more virtual elements associated with functions to be performed by a component of the aircraft. The method can include receiving data indicative of an actual user interaction with the touch screen display device. The method can include receiving data indicative of an intended user interaction. The method can include receiving data indicative of a sensed vibration. The method can include determining a corrected user interaction corresponding to a selected virtual element based on the data received. The method can also include sending one or more command signals to one or more components to perform a function associated with the selected virtual element.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.