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Journal of the Korea Institute of Military Science and Technology 1999;2(2):218-225.
A Study on the Circular Error Probability of Short-Range Rocket with Parachute
,
낙하산을 갖는 단거리 발사체의 오차분석
김찬수, 조요한
국방과학연구소
Abstract
This paper contains the computational simulation of a free rocket with a parachute and the development of a firing table for each range. To obtain the trajectory of the rocket, 6 DOF model of rocket with parachute was generated and the wind tunnel test was done for the input parameters. Good agreement was obtained between the analysis of trajectory and the flight test result. Also the trajectory error analysis was performed by the Monte Carlo simulation. As a result of simulation, the CEP(Circular Error Probability) of the firing table was calculated.
Key Words: Firing Table, Monte Carlo simulation, CEP(Circular Error Probability)


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