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无人直升机自动着舰导引控制设计与验证
引用本文:赖水清,严峰,王青林.无人直升机自动着舰导引控制设计与验证[J].直升机技术,2014(2):29-35.
作者姓名:赖水清  严峰  王青林
作者单位:中国直升机设计研究所,江西景德镇333001
摘    要:针对无人直升机自动着舰的特点和需求,研究着舰导引轨迹生成,进行着舰导引轨迹跟踪控制设计,并通过仿真和飞行试验验证跟踪控制的精确性。

关 键 词:无人直升机  着舰导引控制

Design and Validate of Flight Path Control of Automatic Carrier Landing for Unmanned Helicopter
Authors:LAI Shuiqing  YAN Fengi  WANG Qinglin
Institution:( China helicopter Research and development Institute, Jingdezhen 333001, China)
Abstract:This paper aimed at the characteristics and requirements of unmanned helicopter auto-matic carrier landing, the guidance path create of automatic carrier landing was researched, then the design of automatic carrier landing guidance track control was developed, finally the control precision of automatic carrier landing guidance track was validated by simulation and flight test.
Keywords:unmanned helicopter  autonomous carrier  landing control
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