Initial design study of existing flight control system of RPH and feasibility study of implementing HHC on the SH-60B

Approved for public release; distribution unlimited. === The paper reports on two subjects, first the initial design study of a Remotely Piloted Helicopter's flight control system and secondly a feasibility study of implementing Higher Harmonic Control on the SH-60B aircraft. Described for the...

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Main Author: Webb, Charles David
Other Authors: Wood, E. Roberts
Published: Monterey, California: Naval Postgraduate School 2013
Online Access:http://hdl.handle.net/10945/34955
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spelling ndltd-nps.edu-oai-calhoun.nps.edu-10945-349552015-02-03T15:54:58Z Initial design study of existing flight control system of RPH and feasibility study of implementing HHC on the SH-60B Webb, Charles David Wood, E. Roberts Howard, Richard M. Naval Postgraduate School (U.S.) Aeronautics and Astronautics Approved for public release; distribution unlimited. The paper reports on two subjects, first the initial design study of a Remotely Piloted Helicopter's flight control system and secondly a feasibility study of implementing Higher Harmonic Control on the SH-60B aircraft. Described for the former is a complete study of stiffness constants, system freeplays and power requirements needed to provide Higher Harmonic Control to the Remotely Piloted Helicopter. The later gives practical design considerations for four alternate mechanicalhydraulic designs. The Remotely Piloted Helicopter Higher Harmonic Control work is an ongoing project at the Naval Postgraduate School and the SH-60B work is an initial study which is currently being evaluated at the Naval Air Test Center. 2013-08-01T21:15:58Z 2013-08-01T21:15:58Z 1990-09 Thesis http://hdl.handle.net/10945/34955 This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. As such, it is in the public domain, and under the provisions of Title 17, United States Code, Section 105, it may not be copyrighted. Monterey, California: Naval Postgraduate School
collection NDLTD
sources NDLTD
description Approved for public release; distribution unlimited. === The paper reports on two subjects, first the initial design study of a Remotely Piloted Helicopter's flight control system and secondly a feasibility study of implementing Higher Harmonic Control on the SH-60B aircraft. Described for the former is a complete study of stiffness constants, system freeplays and power requirements needed to provide Higher Harmonic Control to the Remotely Piloted Helicopter. The later gives practical design considerations for four alternate mechanicalhydraulic designs. The Remotely Piloted Helicopter Higher Harmonic Control work is an ongoing project at the Naval Postgraduate School and the SH-60B work is an initial study which is currently being evaluated at the Naval Air Test Center.
author2 Wood, E. Roberts
author_facet Wood, E. Roberts
Webb, Charles David
author Webb, Charles David
spellingShingle Webb, Charles David
Initial design study of existing flight control system of RPH and feasibility study of implementing HHC on the SH-60B
author_sort Webb, Charles David
title Initial design study of existing flight control system of RPH and feasibility study of implementing HHC on the SH-60B
title_short Initial design study of existing flight control system of RPH and feasibility study of implementing HHC on the SH-60B
title_full Initial design study of existing flight control system of RPH and feasibility study of implementing HHC on the SH-60B
title_fullStr Initial design study of existing flight control system of RPH and feasibility study of implementing HHC on the SH-60B
title_full_unstemmed Initial design study of existing flight control system of RPH and feasibility study of implementing HHC on the SH-60B
title_sort initial design study of existing flight control system of rph and feasibility study of implementing hhc on the sh-60b
publisher Monterey, California: Naval Postgraduate School
publishDate 2013
url http://hdl.handle.net/10945/34955
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