A simple method of obtaining range and velocity information has long been sought for numerous applications.1One such application concerns itself with detecting the presence of an obstacle in the path of a moving vehicle, the distance to it, and the rate of closure. Since the ranging capabilities of such a system must include an approach…
IEEE Transactions on Aerospace and Navigational Electronics Template
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About the IEEE Transactions on Aerospace and Navigational Electronics format
IEEE Transactions on Aerospace and Navigational Electronics is a peer-reviewed journal published by IEEE, covering Diverse Scientific and Economic Studies, Human auditory perception and evaluation, Inertial Sensor and Navigation.
| Publisher | IEEE |
|---|---|
| Reference style | Numbered (IEEE) Numbered — [1], [2] in the text [1] A. Smith, B. Jones, and C. Lee, "A representative article title," IEEE Transactions on Aerospace and Navigational Electronics, vol. 12, no. 3, pp. 45–58, 2023.
Formats any DOI in IEEE Transactions on Aerospace and Navigational Electronics style. No sign-up. |
| Publishes research in | Diverse Scientific and Economic Studies Human auditory perception and evaluation Inertial Sensor and Navigation Advanced Control and Stabilization in Aerospace Systems Legal case studies and regulations |
| ISSN | 0096-1957 |
| h-index | 12 |
| i10-index | 14 |
| Total citations | 484 |
| Top institutions publishing here | Federal Aviation Administration |
| Journal website | books.google.com |
| You get | A submission-ready PDF and the editable LaTeX source — ready to submit. |
Papers published in IEEE Transactions on Aerospace and Navigational Electronics per year
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Most-cited papers in IEEE Transactions on Aerospace and Navigational Electronics
A mathematical model for the error distribution of the best estimate of position of a vehicle as determined from a set of simultaneous measurements of times of arrival of electromagnetic waves from an arbitrary number of ground stations is obtained. The major and minor axes of the error ellipse, as well as the angle that…
The earth's horizon provides an important and conspicuous basis for the development of self-contained systems for earth-satellite navigation. The present paper investigates horizonbased navigational systems in which the requirement for vehicular yaw stabilization is not imposed. This permits the development of a variety of navigational techniques which generally fall within one of the following divisions:…
This paper describes a study of the statistical unlock characteristics of the commonly used optimum type II phase-locked loop taking into account the nonlinearity of the phase detector. The unlock behavior is investigated by simulating the loop with random noise inputs on a digital computer. A criterion of loop unlock is evolved using the phase…
A philosophy for the synthesis of a very accurate inertial navigation system is developed here. First, the requirements for a spherical earth navigator are determined, and the basis for a navigator error analysis is developed through the use of mathematical error models. Four types of redundant information are then considered in sequence: external speed information,…