A Study to Determine the Feasibility of a Self-optimizing Automatic Flight Control System
Author: Aeronutronic Ford Corporation
Publisher:
Published: 1960
Total Pages: 130
ISBN-13:
DOWNLOAD EBOOKRead and Download eBook Full
Author: Aeronutronic Ford Corporation
Publisher:
Published: 1960
Total Pages: 130
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1962
Total Pages: 138
ISBN-13:
DOWNLOAD EBOOKAuthor: Defense Documentation Center (U.S.)
Publisher:
Published: 1963
Total Pages: 194
ISBN-13:
DOWNLOAD EBOOKAuthor: David M. Jones
Publisher:
Published: 1962
Total Pages: 1028
ISBN-13:
DOWNLOAD EBOOKA symposium on Aerothermoelasticity was held to present the latest significant developments in each scientific area and engineering area that comprise the component parts of this technology. New and significant contributions were presented in four technical areas consisting of dynamic aerothermoelasticity (flutter), stability and control, thermodynamics and aerodynamics (or aerothermodynamics), and structures including material and construction concepts. Categories important and significant to each technical area are discussed state-of-the-art wise. In addition, 26 separate papers are given on items of special importance.
Author: Herner and Company
Publisher:
Published: 1961
Total Pages: 398
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1964
Total Pages: 520
ISBN-13:
DOWNLOAD EBOOKAuthor: P. C. Gregory
Publisher:
Published: 1959
Total Pages: 474
ISBN-13:
DOWNLOAD EBOOKAuthor: Lincoln Laboratory. Library
Publisher:
Published: 1961
Total Pages: 34
ISBN-13:
DOWNLOAD EBOOKAuthor: John H. Blakelock
Publisher: John Wiley & Sons
Published: 1991-09-03
Total Pages: 668
ISBN-13: 9780471506515
DOWNLOAD EBOOKThis Second Edition continues the fine tradition of its predecessor by exploring the various automatic control systems in aircraft and on board missiles. Considerably expanded and updated, it now includes new or additional material on: the effectiveness of beta-beta feedback as a method of obtaining coordination during turns using the F-15 as the aircraft model; the root locus analysis of a generic acceleration autopilot used in many air-to-air and surface-to-air guided missiles; the guidance systems of the AIM-9L Sidewinder as well as bank-to-turn missiles; various types of guidance, including proportional navigation and line-of-sight and lead-angle command guidance; the coupling of the output of a director fire control system into the autopilot; the analysis of multivariable control systems; and methods for modeling the human pilot, plus the integration of the human pilot into an aircraft flight control system. Also features many new additions to the appendices.