Application Of Statistical Theory To Beam Rider Guidance In The Presence Of Noise

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Application of Statistical Theory to Beam-rider Guidance in the Presence of Noise

Author : Elwood C. Stewart
Publisher : Unknown
Page : 54 pages
File Size : 45,8 Mb
Release : 1955
Category : Aeronautics
ISBN : UOM:39015086432492

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Application of Statistical Theory to Beam-rider Guidance in the Presence of Noise by Elwood C. Stewart Pdf

A study has been made of the application of Newton's modification of the Wiener filter theory to the optimization of a beam-rider guidance system operating in the presence of glint noise. Target and missile motions are assumed to be coplanar.

Application of Statistical Theory to Beam-rider Guidance in the Presence of Noise

Author : Elwood C. Stewart,United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 40 pages
File Size : 53,5 Mb
Release : 1955
Category : Charts, diagrams, etc
ISBN : OCLC:712674940

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Application of Statistical Theory to Beam-rider Guidance in the Presence of Noise by Elwood C. Stewart,United States. National Advisory Committee for Aeronautics Pdf

A study has been made of the application of Wiener filter theory to the design of a beam-rider guidance system operating in the presence of glint noise. Target and missile motions are restricted to the same plane. The Wiener theory is then used to establish the theoretical lower limit of root-mean-square error and the corresponding desired transfer-function characteristics. It is shown that although the practical achievement of these results is restricted by saturation effects, the theory is useful, with suitable modifications, as a guide in system design. Such modifications have been applied to the design of systems for which the optimum filtering is placed either in the missile-control system or in the tracking radar. The error performance of these systems for different noise magnitudes is presented. Other considerations such as servo energy requirements are briefly discussed.

Technical Note - National Advisory Committee for Aeronautics

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 1132 pages
File Size : 54,7 Mb
Release : 1958
Category : Aeronautics
ISBN : RUTGERS:39030037544667

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Technical Note - National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf

Research Abstracts and Reclassification Notice

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 716 pages
File Size : 50,7 Mb
Release : 1956
Category : Aeronautics
ISBN : OSU:32435062280276

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Research Abstracts and Reclassification Notice by United States. National Advisory Committee for Aeronautics Pdf

NACA Conference on High-Speed Aerodynamics

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 678 pages
File Size : 43,7 Mb
Release : 1958
Category : Aerodynamics, Supersonic
ISBN : UOM:39015007668018

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NACA Conference on High-Speed Aerodynamics by United States. National Advisory Committee for Aeronautics Pdf

NASA Technical Note

Author : Anonim
Publisher : Unknown
Page : 1188 pages
File Size : 55,7 Mb
Release : 1961
Category : Aeronautics
ISBN : UOM:39015006073640

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NASA Technical Note by Anonim Pdf

NASA Memorandum

Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 520 pages
File Size : 42,7 Mb
Release : 1959
Category : Aeronautics
ISBN : UOM:39015006108990

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NASA Memorandum by United States. National Aeronautics and Space Administration Pdf

Dynamic Stability of Vehicles Traversing Ascending Or Descending Paths Through the Atmosphere

Author : Murray Tobak,H. Julian Allen
Publisher : Unknown
Page : 664 pages
File Size : 45,5 Mb
Release : 1958
Category : Ballistic missiles
ISBN : STANFORD:36105024832540

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Dynamic Stability of Vehicles Traversing Ascending Or Descending Paths Through the Atmosphere by Murray Tobak,H. Julian Allen Pdf

An analysis is given of the oscillatory motions of vehicles which traverse ascending and descending paths through the atmosphere at high speed. The specific case of a skip path is examined in detail, and this leads to a form of solution for the oscillatory motion which should recur over any trajectory. The distinguishing feature of this form is the appearance of the Bessel rather than the trigonometric function as the characteristic mode of oscillation.

Index of NACA Technical Publications

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 388 pages
File Size : 49,7 Mb
Release : 1959
Category : Aeronautics
ISBN : UCBK:C029901327

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Index of NACA Technical Publications by United States. National Advisory Committee for Aeronautics Pdf

Ordnance Corps Pamphlet

Author : United States. Army. Ordnance Corps
Publisher : Unknown
Page : 298 pages
File Size : 46,5 Mb
Release : 1962
Category : Electronic
ISBN : STANFORD:36105126755565

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Ordnance Corps Pamphlet by United States. Army. Ordnance Corps Pdf

Ordnance Engineering Design Handbook

Author : Anonim
Publisher : Unknown
Page : 306 pages
File Size : 55,9 Mb
Release : 1968
Category : Guided missiles
ISBN : MINN:31951D03437895P

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Ordnance Engineering Design Handbook by Anonim Pdf

Creep Deformation Patterns of Joints Under Bearing and Tensile Loads

Author : E. G. Bodine,R. L. Carlson,G. K. Manning
Publisher : Unknown
Page : 668 pages
File Size : 53,9 Mb
Release : 1957
Category : Deformation (Mechanics)
ISBN : STANFORD:36105024832367

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Creep Deformation Patterns of Joints Under Bearing and Tensile Loads by E. G. Bodine,R. L. Carlson,G. K. Manning Pdf

The objective of the present investigation was to study the interaction of bearing and tensile loads on the creep behavior of joints. To achieve this objective, a simplified model was employed which contained many of the features found in riveted connections. Through the use of this simulated joint, an analysis of complex regions in actual joints could be effected. In the study, results for a number of tensile-to-bearing load ratios were obtained, and the results were analyzed.