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Aerospace and Navigational Electronics, IRE Transactions on

Issue 1 • Date March 1962

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Displaying Results 1 - 15 of 15
  • IRE Transactions on Aerospace and Navigational Electronics

    Publication Year: 1962 , Page(s): c1
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  • IRE Professional Group on Aerospace and Navigational Electronics

    Publication Year: 1962 , Page(s): c2
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  • Table of contents

    Publication Year: 1962 , Page(s): 1
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  • The Editor Reports

    Publication Year: 1962 , Page(s): 2
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  • NAECON Luncheon Address

    Publication Year: 1962 , Page(s): 3 - 6
    Save to Project icon | Request Permissions | Click to expandAbstract | PDF file iconPDF (888 KB)  

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  • A New Guiding and Tracking System

    Publication Year: 1962 , Page(s): 7 - 10
    Cited by:  Papers (13)  |  Patents (7)
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    A new application of the near-field theory is described which permits determination of the relative bearing of one object with respect to another by a simple phase measurement without an additional reference signal. The same instrument is used to measure distance between the objects. The angle indication is independent of distance. View full abstract»

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  • Airborne Doppler Radar Navigation of Jet Transport Aircraft

    Publication Year: 1962 , Page(s): 11 - 20
    Cited by:  Papers (6)
    Save to Project icon | Request Permissions | Click to expandAbstract | PDF file iconPDF (3597 KB)  

    Trans World Airlines will pioneer use of Doppler radar as a primary means of transport aircraft navigation over the North Atlantic. This paper summarizes flight test results using dual Doppler radar sensors and dual Doppler navigation computers on Boeing 707 long range aircraft. Test flights have been flown over TWA's North Atlantic routes for almost two years to ¿prove-in¿ the Doppler system. View full abstract»

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  • Criterion for Angular Noise in Star-Lock Systems

    Publication Year: 1962 , Page(s): 21 - 23
    Cited by:  Papers (2)
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    This paper shows that, if the signal-to-noise power ratio (S/N) is found for any steady deviation ¿ of a parameter from its required value, then in a closed-loop linear servo system, the actual rms variation of the parameter from its required value due to noise cannot exceed the rms value: View full abstract»

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  • FM Star-Lock System Using Mask with Linear Sectors

    Publication Year: 1962 , Page(s): 24 - 34
    Cited by:  Papers (2)
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    This is a known type of system in which a suitable rotating element in the optical system causes the image of the star field to nutate over the surface of a mask divided into alternative sectors of opaque and transparent material. When the lock star is on the axis of the entry optical system, the lock-star image traverses a circular path on the mask concentric with the mask giving rise to an unvar... View full abstract»

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  • FM Star-Lock System Using Mask with Spiral Sectors

    Publication Year: 1962 , Page(s): 35 - 47
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    This system is identical with the FM system using a linear mask except that the sectors of the mask are bounded by spirals. The value of ¿ = (r/R)(S/N)-1/2 is derived for the case of spiral masks of three kinds. View full abstract»

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  • Abstracts

    Publication Year: 1962 , Page(s): 48
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  • PGANE News

    Publication Year: 1962 , Page(s): 49
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  • Contributors

    Publication Year: 1962 , Page(s): 50
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  • Suggestions to Authors

    Publication Year: 1962 , Page(s): 50a
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  • Institutional listings

    Publication Year: 1962 , Page(s): 50b
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Aims & Scope

This Transactions ceased publication in 1962. The new retitled publication is IEEE Transactions on Aerospace and Electronic Systems.

Full Aims & Scope