Coriolis indicator for situational awareness

Details Coriolis indicator for situational awareness Coriolis indicator for situational awareness

1992-08-25

1994-10-04

Black, Thomas G.

Boots, shoes, and leggings

73505, 73510, 364578, G01P 904

Patent

active

053532260

ABSTRACT:
A system for indicating the presence of Coriolis accelerations within an aircraft which might affect pilot perception of aircraft attitude and spatial orientation, which comprises sensors for measuring vehicle angular position, rotations and velocities operatively connected to an onboard computer program which calculates the Coriolis accelerations according to an analysis presented herein and presented on a display to the pilot.

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"A Study of Supermaneuverable Flight Trajectories Through Motion Field Simulation of a Centrifuge Simulator", by D. W. Reppenger J. Dynamic Systems, Measurment and Control, 144:6, 271 (Jun. 1992).

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