Methodological aspects of effectiveness evaluation of active limitation systems of marginal aircrafts flight regimes in mathematical modeling and in flight testing

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Abstract

In the system of measures to ensure flight safety and enhance the combat capabilities of modern aircraft, importance is attached to equipping them with appropriate technical devices. This article is devoted to the analysis of the use on aircraft of active systems of limiting the limiting flight regimes intended to prevent the aircraft from exiting the permissible values ​​of the angle of attack (overload) during its combat use. The paper presents a mathematical model of the movement of an aircraft with an active automatic machine limiting flight limits, which allows a preliminary assessment of the behavior of an aircraft with a working limiter on various flight modes, the effect of changes within the limits of operational tolerances of the parameters of the automatic machine, aircraft centering, etc. evaluation of active automata limit the limiting flight modes in flight tests.

Author Biography
  1. V. O. Smirnov, Central Scientific Research Institute of Armament and Military Equipment of the Armed Forces of Ukraine

    Candidate of Technical Sciences
    Senior Researcher

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Published
2019-03-26
Section
AIRCRAFT ARMAMENT & FACILITIES
License
Creative Commons License

This work is licensed under a Creative Commons Attribution 4.0 International License.

How to Cite

Methodological aspects of effectiveness evaluation of active limitation systems of marginal aircrafts flight regimes in mathematical modeling and in flight testing. (2019). Weapons and Military Equipment, 21(1), 54-58. https://doi.org/10.34169/2414-0651.2019.1(21).54-58