Missile Mathematical Model and System Design

  • Papp István
doi: 10.32565/aarms.2017.1.3

Abstract

Recently, aerospace (flight) engineers, having more solid mathematical backgrounds, have become familiar with the newest results in control theory and are able not only to formulate control problems but also solve them without attracting the attention of control experts. Moreover, they try to apply new results in control theory to specific aerospace and missile guidance problems. As a result, control theory is losing its biggest supplier and, to a certain degree, this slows down its progress.

Keywords:

mathematical control missile equations of motion

How to Cite

Papp, I. (2017) “Missile Mathematical Model and System Design”, AARMS – Academic and Applied Research in Military and Public Management Science. Budapest, 16(1), pp. 29–35. doi: 10.32565/aarms.2017.1.3.

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