An approach to design of the rudder—drive system taking into account the aeroelastic characteristics of the rudder is proposed. Mathematical models are developed that are used to solve problems of the rudder design parameters selection and the rudder—drive system stability analysis. An example of design of the rudder—drive system of the air-to-air unmanned aerial vehicle is given.

中文翻译：

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一种考虑气动弹性稳定性要求的舵驱动系统设计方法

提出了一种考虑舵的气弹特性的舵驱动系统的设计方法。开发了用于解决舵设计参数选择和舵-驱动系统稳定性分析问题的数学模型。给出了空对空无人机的舵机驱动系统的设计实例。