WorldCat Identities

Innis, Robert C.

Overview
Works: 4 works in 14 publications in 1 language and 85 library holdings
Classifications: TL521.3, 629.1325240426
Publication Timeline
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Most widely held works by Robert C Innis
Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches by W. S Hindson( Book )

9 editions published in 1981 in English and held by 66 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 2 WorldCat member libraries worldwide

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

Flight-Test Evaluation of STOL Control and Flight Director Concepts in a Powered-Lift Aircraft Flying Curved Decelerating Approaches (Evaluation des Essais en Vol d'un Directeur de Vol et des Commands d'un Adac portance Assistee evoluanten Approche Curviligne en Deceleration)( Book )

1 edition published in 1981 in English and held by 1 WorldCat member library worldwide

Flight tests were carried out to assess the feasibility of piloted steep, curved, and decelerating-approach profiles in powered-lift STOL aircraft. Several STOL control concepts representative of a variety of aircraft were evaluated in conjunction with suitably designed flight directors. The tests were carried out in a real navigation environment, employed special electronic cockpit displays, and included the development of operational procedures considered appropriate to this class of aircraft. Data are presented describing the performance achieved and the control utilization involved in flying 180 deg turning, descending, and decelerating-approach profiles to landing. The results suggest that such moderately complex piloted instrument approaches may indeed be feasible from a pilot acceptance point of view, given an acceptable navigation environment. Systems with the capability of those used in this experiment can provide the potential of achieving instrument operations on curved, descending, and decelerating landing approaches to weather minima corresponding to CTOL Category II criteria, while also providing a means of realizing more efficient operations during visual flight conditions. (Author)
 
Audience Level
0
Audience Level
1
  Kids General Special  
Audience level: 0.68 (from 0.67 for Flight-tes ... to 0.99 for Flight-Tes ...)

Languages
English (14)