高速旋回潜体对差动舵角运动响应研究  

Research on motion response of detach plane rudder about submarine cycling in high speed

作　　者：张平[1] 刘常波[1] 胡坤[1] 田炳丽[1] ZHANG Ping;LIU Chang-bo;HU Kun;TIAN Bing-li(Navy Submarine Academy,Qingdao 266199,China)

机构地区：[1]海军潜艇学院,山东青岛266199

出　　处：《舰船科学技术》2020年第7期107-111,共5页Ship Science and Technology

摘　　要：分离式舵不同操舵方式可产生差动舵角,目前,针对差动舵角对高速机动潜体的旋回运动特性研究尚未完全展开。为此,本文以分离式舵6DOF运动方程为基础,研究差动舵角对高速旋回潜体运动姿态、特别是横倾的控制能力,比较不同差动舵角对潜体定深、变深运动姿态的影响。研究结果表明,差动舵角对于潜体高速旋回时的运动姿态、特别是横倾有较强的控制、抑制能力。Differential plane angle can be produced by different maneuvering modes of detach plane.At present,the cycle study of motion characteristics about detach plane angle has not been fully developed.Consequently,this paper bases on the 6DOF motion equation of detach plane to research the motion posture of submarine and the controlling capability of heel in high speed,and compare the influence of detach plane to the submarine in certain depth and in changing depth.The research show that detach plane angle has strong control and restraint ability for attitude control,especially for heel control of submarine in high speed.

关 键 词：差动舵角 高速旋回 横倾 阶跃控制 

分 类 号：U674[交通运输工程—船舶及航道工程]