Implicit guidance using linear tangent pitch program

선형 탄젠트 피치 프로그램을 이용하는 Implicit 유도

  • 진재현 (한국과학기술원 항공우주학과) ;
  • 탁민제 (한국과학기술원 항공우주학과)
  • Published : 1992.10.01

Abstract

Implicit guidance algorithm can deal with the trajectory error rapidly, but it has to save much data. If, however, the control variable is represented by a specific function form, a few parameters will suffice to define the control variable. In this paper, we study the method of updating the parameters of the control function for the reduction of trajectory errors. The method proposed here does not require much memory for guidance.

Keywords