Minimizing coriolis-tumbling intensity in a centrifuge-based-flight simulator
US9214092B2 · kind B2 · utility
Assignee
Inventor
Key dates
| Filing date | Mar 15, 2013 |
| Grant date | Dec 15, 2015 |
| Priority date | — |
| Expiry date | Jun 30, 2033 |
Classification
- Technology area (CPC G)Physics
- CPC primaryG09B9/12
- WIPO fieldControl
- WIPO sectorInstruments
Abstract
A system and method for minimizing or eliminating Coriolis-tumbling sensations on a trainee in a centrifuge-based simulator is described. In one example methodology, a simulator transitions its rate of rotation to replicate flight conditions in which G-forces are unloaded on a trainee from a first-G-force value to a nominal-G-force value. Before reaching the nominal-G-force value, an intermediate-G-force value—which is more than the nominal-G-force value, but less than the first-G-force value—is imparted and maintained on the trainee for a suitable duration of time. This intermediate-G-force value may be determined based on several factors including: (i) the angle of rotation of a gondola at during the first-G-force value, and/or (ii) the first-G-force value. After the intermediate-G-force value is imparted and maintained for a suitable duration of time, the G-forces imparted on the trainee may be further unloaded till the nominal-G force value is reached.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.