A.A.Tomilov1, A.V. Potudinsky2, I.K. Makarov3

1–3 Military training scientific center of the «Air Force Academy n.a. Professor N.E. Zhukovsky and Yu.A. Gagarin» (Voronezh, Russian Federation)
2 alepaha@yandex.ru

Safety is ensured, including the safe landing of the aircraft. A short landing run without a skid is achieved by the necessary preparation of the runway, a serviceable braking system, anti-skid automation and take-off and landing devices of the aircraft. Standard operation of anti-skid automatics should be able to cope with constant non-linearity of movement and atmospheric interference on the surface of the runway, as well as adjust the wheel slip coefficient to ensure reliable operation of the braking system. The need to develop technical solutions in the field of expanding the operational capabilities of diagnostic tools for anti-youth automation of the aircraft braking system is determined by regular aviation incidents, related to failures of anti-skid devices, including their incorrect setting before installation on the aircraft landing gear wheel, which leads to serious consequences – increased wear of the wheel tire surface and its possible destruction, including an emergency landing due to loss of control over the aircraft.

The purpose of the work is to simulate the youth situation of the aircraft during landing, to study the problem, to increase the efficiency, reliability of the results of diagnosing devices and automata of the aircraft braking system.

This article discusses the main external and operational factors affecting the dynamics and nature of the aircraft's run along the runway, the model of aircraft movement with the influence of aerodynamic forces on it, the model of tire friction on the ground, and also proposes a method for diagnosing anti-youth automation of the aircraft braking system.

Tomilov A.A., Potudinsky A.V., Makarov I.K. Simulation of the landing situation of an aircraft and the problems of diagnosing anti-skid devices. Science Intensive Technologies. 2024. V. 25. № 5. P. 46−54. DOI: https://doi.org/ 10.18127/j19998465-202405-04 (in Russian)

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