Significant improvements in performance can be obtained if automatic flight control system is given task of improving handling qualities of basic aircraft and augmenting damping of flexible airframe; summary of data on passenger comfort obtained from motion simulators, routine airline operations, and military flight test data; passenger-comfort boundary that covers frequency range of .2-100 cps is defined; criteria for evaluating alleviation of structural fatigue are determined; recommendations made.
Requirements for flight control system of supersonic transport
SAE -- Paper
SAE Meeting ; 1963 Control equipment
1963
25 pages
Aufsatz (Konferenz)
Englisch
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Requirements for the Flight Control System of a Supersonic Transport*
SAE Technical Papers | 1963
|Effects of supersonic transport flight characteristics on performance requirements
Engineering Index Backfile | 1963
|Flight Control System Design for Supersonic Transport
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|Supersonic transport propulsion requirements
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|THE EFFECTS OF SUPERSONIC TRANSPORT FLIGHT CHARACTERISTICS ON PERFORMANCE REQUIREMENTS
SAE Technical Papers | 1963
|