一种位标器陀螺跟踪系统的快速起旋控制设计  

A new design of fast spin up control on seeker gyro tracking system

作　　者：李正阳 王烁[2] 蔡文硕 Li Zhengyang;Wang Shuo;Cai Wenshuo(Introduction of Institute of Teleommunication and Navigation Satellites China Aadmyof Space Technoogy Bejing 100094,China;China Academy of Space Technology,Beijing 100094,China)

机构地区：[1]中国空间技术研究院通信与导航卫星总体部,北京100094 [2]中国空间技术研究院,北京100094

出　　处：《电子测量技术》2022年第14期43-49,共7页Electronic Measurement Technology

摘　　要：现代战争中,红外制导导弹的地位不断提高,世界各国均高度重视对红外制导导弹的研制,导引头位标器作为导弹制导控制的关键部件,其性能对导弹作战能力具有决定性的影响。本文针对某型导引头位标器陀螺跟踪系统中的悬浮、起旋、稳速控制问题进行了分析研究,提出了一种新的控制方法,实现了位标器陀螺的高可靠快速起旋控制,并完成了试验验证。试验结果表明,本文的快速起旋控制设计能够确保高可靠的同时大幅缩短位标器的启动时间,能够有效提升导弹的作战性能。In modern warfare, the status of infrared-guided missiles is increasing, and the most countries in the world attach great importance to the development of infrared-guided missiles. The performance of the seeker gyro, as a key component of missile guidance control, has a decisive influence on the operational capability of missiles. In this paper, we analyze and study the suspension, spin up and speed stabilization control problems in the gyroscopic tracking system of a certain type of seeker, and propose a new control method to realize the highly reliable and fast spin up control of the seeker gyro and complete the test verification. The experimental results show that the fast spin up control design of this paper can ensure the high reliability and shorten the start-up time of the seeker at the same time, which can effectively improve the operational performance of the missile.

关 键 词：红外导引头位标器 陀螺 空空导弹 起旋 

分 类 号：TP2[自动化与计算机技术—检测技术与自动化装置]