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Aerospace Instrument-Making

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FEATURES OF TESTING HIGHLY AUTOMATED AIRCRAFT IN ASYMMETRIC CONFIGURATION
D.A. Golovaty, S.V. Nikolaev

The article is devoted to the issue of assessing the characteristics of stability and controllability of an aircraft with an asymmetric configuration in tests. Variants of expert systems are proposed for assessing the stability and controllability characteristics of an aircraft in an asymmetric state both on the basis of the existing regulatory and technical base and on the basis of flight test results. A feature of the proposed expert systems is the output variable, which is an artificial criterion for assessing stability and controllability in an asymmetric state, based on a repeatedly verified scale of pilot ratings.
Keywords: aviation, aviation technology, asymmetry, aircraft testing, expert system.


DOI: 10.25791/aviakosmos.8.2023.1354

Pp. 13-22.

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