WorldCat Identities

Hindson, W. S.

Overview
Works: 25 works in 45 publications in 1 language and 566 library holdings
Roles: Author
Classifications: TL521.3.T4, 629.1325240426
Publication Timeline
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Most widely held works by W. S Hindson
Analytical and flight investigation of the influence of rotor and other high-order dynamics on helicopter flight-control system bandwith by Robert T. N Chen( Book )
1 edition published in 1985 in English and held by 81 WorldCat member libraries worldwide
Acoustic flight tests of rotorcraft noise-abatement approaches using local differential GPS guidance by Robert T. N Chen( Book )
1 edition published in 1995 in English and held by 78 WorldCat member libraries worldwide
In-flight simulation investigation of rotorcraft pitch-roll cross coupling by Douglas C Watson( Book )
1 edition published in 1988 in English and held by 77 WorldCat member libraries worldwide
Influence of dynamic inflow on the helicopter vertical response by Robert T. N Chen( Book )
1 edition published in 1986 in English and held by 76 WorldCat member libraries worldwide
A flight-test and simulation evaluation of the longitudinal final approach and landing performance of an automatic system for a light wing loading STOL aircraft by Stuart C Brown( Book )
2 editions published in 1983 in English and held by 72 WorldCat member libraries worldwide
Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches by W. S Hindson( Book )
3 editions published in 1981 in English and held by 67 WorldCat member libraries worldwide
A flight investigation using variable glide path trajectories to compensate for winds and moderate wind shears by W. S Hindson( Book )
4 editions published in 1976 in English and held by 7 WorldCat member libraries worldwide
Modification of V/stol instrument approach geometry as a means of compensating for along-track wind effects by W. S Hindson( Book )
3 editions published between 1973 and 1974 in English and held by 6 WorldCat member libraries worldwide
Estimates of the Lateral Directional Stability Derivatives of a Helicopter From Flight Measurements by National Aeronautical Establishment (Canada)( Book )
2 editions published in 1973 in English and held by 6 WorldCat member libraries worldwide
Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches by W. S Hindson( Book )
3 editions published in 1981 in English and held by 5 WorldCat member libraries worldwide
A summary of joint U.S.-Canadian augmentor wing powered-lift STOL research programs at the Ames Research Center, NASA, 1975-1980 by W. S Hindson( Book )
3 editions published in 1980 in English and held by 3 WorldCat member libraries worldwide
Modification of V by National Aeronautical Establishment (Canada)( Book )
1 edition published in 1974 in English and held by 3 WorldCat member libraries worldwide
Flight Investigation Using Variable Glide Path Trajectories to Compensate For Winds and Moderate Wind Shears by National Aeronautical Establishment (Canada)( Book )
2 editions published in 1976 in English and held by 2 WorldCat member libraries worldwide
Study of Helicopter Roll Control Effectiveness Criteria ( Book )
2 editions published in 1986 in English and held by 2 WorldCat member libraries worldwide
A study of helicopter roll control effectiveness based on closed-loop task performance measurement and modeling is presented. Roll control criteria are based upon task margin, the excess of vehicle task performance capability over the pilot's task performance demand. Appropriate helicopter roll axis dynamic models are defined for use with analytic models for task performance. Both near-earth and up-and-away large-amplitude maneuvering phases are considered. The results of in-flight and moving-base simulation measurements are presented to support the roll control effectiveness criteria offered. This Volume contains the theoretical analysis, simulation results and criteria development. Keywords: Rotorcraft; Helicopter handling qualities. (Author)
Flight-Test Evaluation of Stol Control and Flight Director Concepts in a Powered-Lift Aircraft Flying Curved Decelerating Approaches by National Aeronautical Establishment (Canada)( Book )
2 editions published in 1981 in English and held by 2 WorldCat member libraries worldwide
Estimates of the Lateral-Directional Stability Derivatives of a Helicopter from Flight Measurements (Les Evaluations des Mesures en Vol des Derivees de Stabilite Lateratles-Directionnelles D'un Helicoptere) ( Book )
1 edition published in 1973 in English and held by 1 WorldCat member library worldwide
The lateral-directional stability derivatives for a medium-sized single rotor helicopter have been estimated for three different forward speeds. The analysis technique is based on a least squares quasilinearization method which employs a specially formatted parameter vector so that reliable a priori estimates can be used to assist convergence. An additional unique feature is the procedure adopted to reduce the influence of unknown atmospheric inputs on the parameter estimates by means of a conglomerate analysis of several similar runs. (Author)
Flight experiments using the front-side control technique during piloted approach and landing in a powered-life STOL aircraft by W. S Hindson( Book )
1 edition published in 1982 in English and held by 1 WorldCat member library worldwide
A Flight Investigation using Variable Glide Path Trajectories to Compensate for Winds and Moderate Wind Shears (Etudes en Vol sous Differentes Trajectoires de Descente pour Compenser les Vents et les Cisaillements Moderes du Vent) ( Book )
1 edition published in 1976 in English and held by 1 WorldCat member library worldwide
The influence of wind, wind shears and turbulence on the approach and landing tasks of STOL and V/STOL aircraft has become of significant concern for this evolving class of flight vehicles, particularly during instrument flight operations. Flight experiments have been carried out to assess the considerations in alleviating the effects of along-track, a priori wind, including moderate shears, by adjusting the approach glide path for the conditions of the day. A Bell 205A helicopter modified as an airborne simulator and equipped with a modest programmable guidance and display capability was used for the tests, which were carried out in the operational environment of the Rockcliffe (Ottawa) STOLport. (Author)
 
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Alternative Names
Hindson, William S.
Languages
English (40)