The work was carried out by order of FSUE "GosMKB" Vympel "them. I.I. Toropov, 2002.

In this work, the rocket launch was simulated taking into account the dynamics of the system "aircraft + airplane catapult mechanism + rocket + external environment".The main features of the model: an elastic model of the construction of catapult levers; elastic model of the rocket design; the impact of aerodynamic forces on the aircraft, rocket and catapult levers; the mutual influence of the dynamics of the movement of the aircraft and the rocket.

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The purpose of this study was to determine the dynamic behavior of the mobile launcher when launching missiles. The main features of the model: an elastic model of the chassis platform construction; elastic model of the carriage design; elastic and damping characteristics of the soil.

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The work was carried out by order of JSC "KBP", 2003.

In this work, in the EULER software complex, the rocket launch was simulated taking into account the dynamics of the rocket + container + instrument container + tripod + ground system in three-dimensional space to determine the parameters when the missile leaves the launching container.

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The work was carried out by order of JSC "Kovrov Mechanical Plant", 2002.

Simulation was carried out to assess the accuracy of target damage during automatic shooting with a burst of 3 rounds. The shooting was simulated from the machine, fixed on the stand to simulate the shooting of a person from the "lying down" position. The automaton was modeled as a multimass system of interacting bodies in three-dimensional space with kinematic and force connections.

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The work was carried out by order of Nudelman Precision Engineering Design Bureau, 2004.

Simulation of gun shooting taking into account the dynamics of the "cannon + tower chassis + supporting legs + ground" system in three-dimensional space to determine the accuracy of the shooting. The main features of the model: an elastic model of the chassis platform construction; elastic model of the construction of supporting legs; elastic model of the tower's supporting and rotating circle; elastic and damping characteristics of the soil.

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In this paper, we simulated the dynamics of the launch of an anti-aircraft missile during abnormal operation of the rocket retention mechanism on the launcher. The purpose of the study was to determine the dynamic loads on the rocket design elements and its equipment.

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The work was carried out at the request of FSUE "Uraltransmash", 1998.

In this work, the EULER software complex simulated the dynamic behavior of the self-propelled artillery gun with shots with different turret angles and vertical elevation angles of the barrel. For design studies, it was assumed that the shots are fired from a stationary position, which is a flat horizontal surface with a rigid base.

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The work was carried out at the request of FSUE "GNPP SPLAV", 2002.

The aim of this work was the development of a parametrized model of a nonrigid rocket to conduct research on its dynamic behavior during flight and exit from the launcher. The developed model is used to assess the accuracy of firing and the development of various technical solutions that ensure the stabilization of the projectile during the flight.

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