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Aeronautical and Navigational Electronics, IRE Transactions on

Issue 3 • Date Sept. 1959

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  • IRE Transactions on Aeronautical and Navigational Electronics

    Publication Year: 1959, Page(s): c1
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  • IRE Professional Group on Aeronautical and Navigational Electronics

    Publication Year: 1959, Page(s): c2
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  • Table of contents

    Publication Year: 1959, Page(s): 157
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  • The Editor Reports

    Publication Year: 1959, Page(s): 158
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  • Vector Principles of Inertial Navigation

    Publication Year: 1959, Page(s):159 - 178
    Cited by:  Papers (1)
    Request permission for commercial reuse | Click to expandAbstract | PDF file iconPDF (4748 KB)

    A vector equation, which is derived from first principles, describes the mechanization of inertial navigation systems for use anywhere in space. A specialized form of this equation applies directly to three-dimensional motion at any speed, any altitude, over an elliptical, rotating earth. The usefulness of this equation is illustrated by working out an example of a system design. Behavior of error... View full abstract»

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  • Position Estimation Using Only Multiple Simultaneous Range Measurements

    Publication Year: 1959, Page(s):178 - 187
    Cited by:  Papers (12)
    Request permission for commercial reuse | Click to expandAbstract | PDF file iconPDF (1557 KB)

    Three-dimensional generalized position-measurement systems are analyzed in this paper. In these systems, target position is obtained by trilateration using only range data collected by a group of v stations located in an arbitrary geometry. The method of maximum likelihood is used to obtain a joint estimator for the target coordinates which makes optimal use of the redundant data when the noise is... View full abstract»

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  • "C.P.I."---A Crash Position Indicator for Aircraft

    Publication Year: 1959, Page(s):187 - 200
    Request permission for commercial reuse | Click to expandAbstract | PDF file iconPDF (7414 KB)

    A novel, light, simple and inexpensive position indicator for crashed aircraft has been developed and subjected to severe tests. A special pulsed transmitter with trickle-charged batteries and an internal antenna is potted in shock-absorbing foam transparent to radio waves and placed inside a special aerofoil. This device, held on the tail of the aircraft, is released automatically upon detection ... View full abstract»

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  • Contributors

    Publication Year: 1959, Page(s): 201
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  • Roster of PGANE Members

    Publication Year: 1959, Page(s):202 - 208
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  • Institutional listings

    Publication Year: 1959, Page(s): 208a
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Aims & Scope

This Transactions ceased publication in 1960. The new retitled publication is IEEE Transactions on Aerospace and Electronic Systems.

Full Aims & Scope