无人直升机自动着舰导引控制设计与验证  

Design and Validate of Flight Path Control of Automatic Carrier Landing for Unmanned Helicopter

作　　者：赖水清[1] 严峰[1] 王青林[1] 

机构地区：[1]中国直升机设计研究所,江西景德镇333001

出　　处：《直升机技术》2014年第2期29-35,共7页Helicopter Technique

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。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.

关 键 词：无人直升机 着舰导引控制 

分 类 号：V249.122[航空宇航科学与技术—飞行器设计]