舰载无人直升机着舰时机判定及复飞程序研究  

作　　者：谢欣宏 

机构地区：[1]中国飞行试验研究院飞机所,陕西西安710089

出　　处：《科技创新与应用》2022年第6期82-85,共4页Technology Innovation and Application

摘　　要：在几何空间受限、海上环境复杂多变的条件下进行着舰,是舰载无人直升机任务作业过程中的核心难点。文章基于舰载无人直升机典型着舰引导飞行剖面,分析无人直升机着舰过程中的主要影响因素、机-控制站-载舰之间的信息互联互通关系和载舰运动预估方法,提出了无人直升机着舰时机判定的核心要素以及无法着舰时能有效规避风险的复飞程序,对后续舰载无人直升机型号进行舰基试飞和作战应用具有重要指导意义。Landing under the conditions of limited geometric space and changeable maritime environment is the core difficulty in the mission operation of the carrier-based unmanned helicopter.Based on the typical landing guidance flight profile of a carrier-based unmanned helicopter,this paper analyzes the main influencing factors during the landing process of the unmanned helicopter,the information interconnection relationship between the aircraft,the control station and the carrier,and the method for predicting the movement of the carrier.This paperputs forward the core elements of the unmanned helicopter landing time determination and the go-around procedure that can effectively avoid the risk when the unmanned helicopter cannot land on the ship,which has important guiding significance for the subsequent ship-based unmanned helicopter models to carry out ship-based test flight and combat applications.

关 键 词：舰载无人直升机 着舰时机 复飞程序 飞行试验 

分 类 号：V217[航空宇航科学与技术—航空宇航推进理论与工程]