Aircraft indicator capable of operation in HSI mode or CDI mode

Measuring and testing – Navigation – Take-off and landing monitors

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116290, 116DIG43, G01C 2100, G09F 900

Patent

active

044676433

ABSTRACT:
An indicator instrument for aircraft may be operated in either of two modes. In an HSI mode, first indicia reflect heading, second indicia reflect selected course, and third indicia reflect course deviation. In a CDI mode, the first indicia reflect selected course, the second indicia assume a fixed position, and the third indicia reflect course deviation. A compass validity signal automatically triggers the changeover from HSI mode to CDI mode.

REFERENCES:
patent: 3538881 (1970-11-01), Fenwick
patent: 3696671 (1972-10-01), Steigleder et al.

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