用于飞行器横滚稳定控制的组合陀螺舵研究

Research of Gyro Rudder Combination on the Aircraft Roll Stability Control

在传统单转子陀螺舵的基础上,通过仿真分析和虚拟试验,对陀螺转子数量、结构参数、组合形式和空间布局等进行了多学科优化设计,形成了一系列多转子组合陀螺舵,突破了传统单转子陀螺舵控制能力较小、应用范围受限的现状,提高了其对飞行器横滚稳定控制的能力;针对几种典型飞行器的约束条件,通过组合陀螺舵的设计应用,使其横滚衰减因子达到0.002以上,具有良好的横滚稳定性,有助于推动组合陀螺舵在航天飞行器领域的应用和创新。

Based on the study of traditional single-rotor gyro rudder,this paper completes multi-disciplinary optimization design on amount,structure parameters,combination form and space distribution of rotors by simulation analysis and virtual experiments,and creates a series of multi-rotors combination gyro rudders which overcome the weakness of traditional single-rotor gyro rudder such as small control force and application range limit,thereby improve the control ability of aircraft roll stability.In addition,according to the constraints of some typical aircrafts,via the optimization design of gyro rudder combination,the damping factor of aircraft roll can be greater than 0.002,thus the aircraft can have fine roll stability which contributes to the application and innovation of gyro rudder combination in the field of tactics aircraft.