Real-Time Simulation Algorithm for an Aircraft and a Missile

  • Ueda, Yukio (Nat'l Defense Academy, JAPAN) ;
  • Baba, Yoriaki (Nat'l Defense Academy, JAPAN) ;
  • Takano, Hiroyuki (Nat'l Defense Academy, JAPAN)
  • Published : 2002.10.01

Abstract

Some integration methods for the linear subsystems are examined and which algorithm is optimal for real-time simulation is considered. First, a number of typical integration methods for a linear time-invariant system are given. Then, the dynamic errors are shown both from the point of view of characteristic root errors and transfer function errors. After that we compute the dynamic errors of integration and choose the appropriate method for each system.

Keywords