Author : T. F. Langham
Publisher :
Page : 116 pages
File Size : 10,21 MB
Release : 1980
Category : Guided missiles
ISBN :
A dynamic derivative sensitivity study was conducted to demonstrate the importance of dynamic derivatives in missile motion simulation studies. Generalized bank-to-turn and yaw-to-turn missile configurations were used with a six-degree-of-freedom linearized stability program. The effects of various dynamic derivatives on missile stability were investigated in both level and turning flight for several Mach numbers and altitude conditions.
Author :
Publisher :
Page : 464 pages
File Size : 16,39 MB
Release : 1995
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 218 pages
File Size : 16,13 MB
Release : 1982-05
Category : Science
ISBN :
Author :
Publisher :
Page : 774 pages
File Size : 27,13 MB
Release : 1982
Category : Aeronautics
ISBN :
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Author :
Publisher :
Page : 760 pages
File Size : 26,26 MB
Release : 1982
Category : Aeronautics
ISBN :
Author : Robert C. Nelson
Publisher :
Page : 464 pages
File Size : 23,31 MB
Release : 1998
Category : History
ISBN :
This edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Author : Steven R. Vukelich
Publisher :
Page : 310 pages
File Size : 37,54 MB
Release : 1981
Category : Guided missiles
ISBN :
This report summarizes the methods available to predict the aerodynamic static, dynamic, and control characteristics of missiles. The methods selected for Missile Datcom development were based upon a criteria which included ease of use, accuracy, utility over a range of flight conditions and cost effective in their use. This report describes the methodology appropriate for the missile designer. An outline of a Missile Datcom handbook is proposed; an automated version is also recommended for development. Those areas presently lacking suitable methodologies are also highlighted. (Author).
Author : James M. Jenista
Publisher :
Page : 148 pages
File Size : 48,86 MB
Release : 1983
Category : Angle of attack (Aerodynamics)
ISBN :
Author : United States. Department of the Air Force
Publisher :
Page : 588 pages
File Size : 37,67 MB
Release : 1972
Category : Guided missiles
ISBN :
Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher :
Page : 2300 pages
File Size : 12,58 MB
Release : 1967
Category : Aeronautics
ISBN :
