제어로봇시스템학회:학술대회논문집

Institute of Control, Robotics and Systems (제어로봇시스템학회)
권호 표지

New guidance law for air-to-air missile

  • Baba, Yoriaki (Department of Aerospace Engineering, National Defense Academy) ;
  • Takehira, Tetsuya (Department of Aerospace Engineering, National Defense Academy)
  • Published : 1993.10.01
Download PDF
⟨ Previous Next ⟩

Abstract

In this paper, a new guidance law for a short-range air-to-air missile with constant thrust is presented. It is essentially based on the concept of proportional navigation. First, the theoretical guidance law is derived. Then, we show the technique for practical implementation of the guidance law. By a computer simulation, it is shown that the new guidance law gives better performance than the conventional proportional navigation.

Keywords