Minimizing Coriolis-Tumbling Intensity in a Centrifuge-Based-Flight Simulator
AssigneeEnvironmental Tectonics Corporation
InventorMichael Charles Newman
Life of this patent
Estimating the term…
Loading patent…
AssigneeEnvironmental Tectonics Corporation
InventorMichael Charles Newman
Estimating the term…
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.
A method for minimizing unpleasant Coriolis effects in a centrifuge-based-flight simulator, comprising:
A system for operating a centrifuge-based-flight simulator, comprising:
Computer-readable media comprising a plurality of programming instructions that, upon execution by one or more processors of a computing system, cause the computing system to instruct a centrifuge-based-flight simulator to
Dependencies are inferred from the claim text.