期刊论文详细信息
Defence Science Journal
Guidance Systems of Fighter Aircraft
P. S. Subramanyam1  Ajai Vohra1  K.N. Rajanikanth1  R.S. Rao1 
[1] Aeronautical Development Agency, Bangalore
关键词: Takeoff guidance;    homing guidance;    speed guidance;    auto switch-over guidance;    desired track guidance;    landing guidance;    slope guidance;    angle of attack;    heads-up-display;    weapon delivery guidance;   
DOI  :  
学科分类:社会科学、人文和艺术(综合)
来源: Defence Scientific Information & Documentation Centre
PDF
【 摘 要 】

Mission performance of a fighter aircraft is crucial for survival and strike capabilities in todays' aerial warfare scenario. The guidance functions of such an aircraft play a vital role in meeting the requirements and accomplishing the mission success. This paper presents the requirements of precision guidance for various missions of a fighter aircraft. The concept of guidance system as a pilot-in-loop system is pivotal in understanding and designing such a system. Methodologies of designing such a system are described.

【 授权许可】

Unknown   

【 预 览 】
附件列表
Files Size Format View
RO201912010139665ZK.pdf 2324KB PDF download
  文献评价指标  
  下载次数:7次 浏览次数:1次