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Telecommunications and Radio Engineering
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ISSN Print: 0040-2508
ISSN Online: 1943-6009

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Telecommunications and Radio Engineering

DOI: 10.1615/TelecomRadEng.v56.i3.40
13 pages

Optimal Processing of Information from Inertial and Satellite Navigation Systems by Analysis after Flight

E. G. Kharin
V. G. Maslennikov
N. B. Vavilova
I. A. Kopylov
A. Ch. Staroverov

ABSTRACT

The algorithm of integral navigational information processing, recorded by the flight tests, is presented. The algorithm is intended to automatic analysis of navigational systems errors' features ( inertial, Doppler inertial, radio equipment of short- and long-range navigation, satellite and so on ) and to the forming of real values of trajectory parameters during the whole flight. The specific features of the algorithm in the complex, known as PC "Etalon", are presented. The metrological estimation of its operational modes is given. The experience of the algorithm use in current time in the airborne software of heavy and high-manuever objects is presented.