HydroLogic Redundant Systems Hydraulic Research and Manufacturing Company

Format:

Conference/Event

Author/Creator:

Wood, D., author.

Conference Name:

NASA Aerospace Vehicle Flight Control Conference (1965-07-13 : Los Angeles, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1965

Summary:

This paper considers redundant systems, starting with overall flight control system requirements, and then proceeds via various possible approaches through to a specific concept and its typical applications. Functional, reliability, and safety aspects of a flight control system which are essential to a good redundant scheme are discussed, and the several approaches are compared. The HydroLogics approach is particularly found to offer a simple, versatile, fast acting, and reliable system, based on sound concept and proven hardware. By taking full advantage of these redundant systems, the true potential of high performance vehicles can be realized

Notes:

Vendor supplied data

Publisher Number:

650575

Access Restriction:

Restricted for use by site license