Results on flight dynamics of an axisymmetric vehicle with a control action in the form of gas jet ejection are reported. The differences in the flight trajectories with and without allowance for the pressure redistribution over the vehicle surface due to transverse gas jet ejection are considered and analyzed. Targeted software is developed on the basis of the equations of motion of a material point in space and rotation of the flying vehicle around its center of mass. The influence of the pressure redistribution over the axisymmetric vehicle surface owing to ejection of a lateral transverse gas jet on the flight trajectory and on the rate of vehicle deviation in terms of the yaw angle is demonstrated.

中文翻译：

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带有横向横向射流喷射的轴对称飞行器的飞行动力学研究

报告了具有气体喷射形式的控制作用的轴对称飞行器的飞行动力学结果。考虑和分析了由于横向气体射流喷射而导致的在车辆表面上的压力变化和不存在的飞行轨迹的差异。针对性软件是根据物质点在空间中的运动方程式以及飞行器绕其质心的旋转方程式开发的。证明了由于横向横向气体射流的喷射而导致的压力重新分布在轴对称车辆表面上对飞行轨迹的影响以及对车辆偏航角偏航率的影响。