Study on The Development of Guidance System Technology for 122-140 mm Artillery Rocket

Ahmad Riyadl, Widianto Nugroho, Ahmad Novi Muslimin, Zaenal Asiqin, Rudi Setiawan, Robertus Heru Triharjanto, Yoni Herdian Yogaswara

Abstract

The increase in rocket Artillery accuracy means there will be fewer rockets to be used to destroy a target. This could reduce the needed budget and risk of weapon mobilization. Therefore, this research investigates the advancement in the guidance system technology for Artillery rockets, especially for 122-140 mm caliber. The objective of the research is to find a direction for the development guidance system for the Indonesian Artillery rocket (RHAN). The research use the descriptive-analytic method, in which data was collected from literature studies and inductive analysis was performed. The data shows two kinds of actuators were used, a canard and thrusters. In canard mode, 2 strategies were used, i.e. with bearing to isolate the roll from the rocket, in which 5 control algorithms were used, and without bearing, which 2 control algorithms were used. In thruster mode, there was 5 control algorithms used. Further analysis shows that the best performance is obtained from 2 modes of the canard strategy with bearing, and 2 modes of the thruster strategy. Therefore, it is concluded that the 4 modes can be used to be implemented in RHAN which needs to be added to the control system.

Keywords

MRLS, Rocket, Control system, Canard, Thruster, Circular Error Probable

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DOI: http://dx.doi.org/10.30536/j.jtd.2021.v19.a3691

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