V/STOL Flight Director Systems

SM_ENV_1970-4880

11/16/1970

Authors
Abstract
Content

In keeping with growing requirements for full instrument flight capability in V/STOL vehicles, development effort has been initiated by Sperry Flight Systems Division to improve the pilot control-display interface. Work has been performed in both the command display area and in testing of various operational flight director modes. This paper describes a three-axis flight director system which provides commands for precise control of helicopter, deflected slipstream STOL, or VTOL attitude and power under instrument conditions to very low ceiling and visibility landings.

Meta TagsDetails
DOI
https://doi.org/10.4050/SM_ENV_1970-4880
Citation
Scott, C., "V/STOL Flight Director Systems," Environmental Effects on VTOL Designs - Arlington, Texas 1970, Arlington, Texas, November 16, 1970, https://doi.org/10.4050/SM_ENV_1970-4880.
Additional Details
Publisher
Published
11/16/1970
Product Code
SM_ENV_1970-4880
Content Type
Technical Paper
Language
English