Performance comparison of the notable acceleration- and angle-based guidance laws for a short-range air-to-surface missile

Autor:	Mustafa Kemal Özgören, Gökmen Mahmutyazicioğlu, Bülent Özkan
Rok vydání:	2017
Předmět:	Surface (mathematics) Engineering General Computer Science business.industry Acceleration Missile Range (aeronautics) Performance comparison Law Proportional navigation Electrical and Electronic Engineering Aerospace engineering business Guidance control short-range missile air-to-surface missile
Zdroj:	Volume: 25, Issue: 5 3591-3606 Turkish Journal of Electrical Engineering and Computer Science
ISSN:	1300-0632 1303-6203
Popis:	Short-range air-to-surface missiles have become globally popular in the last two decades. As a performance driver, the type of guidance law gains importance. In this study, proportional navigation, velocity pursuit, and augmented proportional navigation guidance laws, whose resulting guidance commands take the form of lateral acceleration, are applied to a short-range air-to-surface missile against both stationary and maneuvering ground targets. Body pursuit and linear homing guidance laws, which yield angular commands, are additionally applied. Having completed the relevant computer simulations, we conclude that none of the acceleration- and angle-based guidance laws are absolutely superior to the others.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a44045554f372aaae968b0aaa093b04b https://dergipark.org.tr/tr/pub/tbtkelektrik/issue/35793/400811 Zobrazit plný text záznamu