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 | |
【 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 】
Files | Size | Format | View |
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RO201912010139665ZK.pdf | 2324KB | download |