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本文分析了国内外民用飞机横航向控制增稳系统研究现状,并定义了横航向控制增稳系统架构组成及功能。按照美国军方现行的MIL-HDBK-1797飞行品质评定准则,确定了横航向控制增稳系统品质评定范围及指标,并进一步总结出横航向控制增稳系统的主流设计方法,为我国未来民用飞机横航向控制增稳系统设计开发及飞行品质的评定提供一定的参考。
This paper analyzes the research status of stabilizing system for civil aircraft cross-heading at home and abroad, and defines the structure and function of stabilizing system for transverse navigation. According to the MIL-HDBK-1797 flight quality evaluation criteria of the U.S. military, the range and index of the quality assessment of the augmentation system for transverse navigation are determined, and the mainstream design method of the augmentation system for transverse navigation control is further summarized. Provide some reference for the design and development of flight control augmentation system and the assessment of flight quality.