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1)  carrier landing
着舰
1.
This paper analyzes the physical reasons of that a pilot can not control flight path angle only by controlling aircraft attitude in backside carrier landing situation of low dynamic pressure.
分析了低动压的背面(backside)着舰工作状态下飞行员仅控制飞机姿态无法控制飞行轨迹角的物理原因。
2.
In order to make carrier-based airplane land on a carrier safely along an ideal flight path,the automatic carrier landing system(ACLS) must have the ability to trace the deck motion and restrain air turbulence.
为使舰载飞机沿着理想的下滑轨迹安全着舰,自动着舰系统必须具备跟踪甲板运动和抑制气流扰动的性能。
3.
The Optimization of Parameterized Normal Matrix and the carrier landing guidance control system were introduced.
在介绍正规矩阵参数优化方法和着舰导引控制系统的基础上,为提高舰载飞机的操纵性能,采用智能设计软件IntelDes 3。
2)  carrier approach and landing
进舰着舰
1.
By investigating the critical factors, a simulating model of the carrier approach and landing system was developed based on the carrier-airframe-undercarriage multi-body dynamics system.
简述舰载机进舰着舰过程,建立以航母—舰载机—起落架组成的多体动力学系统为核心的进舰着舰系统仿真模型,并综合能够反映驾驶员和LSO的行为特征的指令模型,同时考虑风场扰动,海浪等外界影响因素。
3)  Carrier aircraft landing
舰载机着舰
1.
Carrier aircraft landing is the key technology of modern carrier/carrier aircraft system, and the carrier aircraft landing simulation system provides an effective approach for carrier aircraft automatic guidance and control research.
舰载飞机着舰是现代航空母舰/舰载飞机系统的关键技术,而舰载飞机着舰仿真系统为研究舰载机着舰自动导引和控制提供了有效的途径。
4)  automatic carrier landing
自动着舰
5)  automatic landing
自动着舰
1.
The paper discusses the design of the automatic landing control system control laws and leading laws.
在考虑大气干扰、舰尾流和甲板运动的条件下,以某飞机为例,对其纵向自动着舰控制系统进行分析、设计与仿真,结果表明采用LQG/LTR方法设计的控制器具有较好的鲁棒性,并且具有良好的效果。
6)  velocity of landing on the warship
着舰速度
补充资料:运输舰
用于输送人员、武器装备、弹药和军需物资的军舰。按运载对象,可分武装人员运输舰、干货运输舰和液货运输舰等。
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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