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J. KIMS Technol > Volume 16(6); 2013 > Article
Journal of the Korea Institute of Military Science and Technology 2013;16(6):739-744.
DOI: https://doi.org/10.9766/KIMST.2013.16.6.739   
Pitch Command Generation Method for Consistent Initial Trajectory of Thrust-Vector-Controlled Vehicle
Yong-In Lee, Dong-Gyun Choe, Tae-Won Hwang
추력벡터제어 비행체의 일관된 탄도 성형을 위한 피치각명령 산출 방법
이용인, 최동균, 황태원
국방과학연구소 1기술연구본부
Abstract
In this paper, we propose a method of generating pitch commands for consistent initial trajectories irrelevant to flight conditions in the initial boosting phase of a thrust-vector-controlled vehicle. After shape assumption of the pitch command profile, parameters of the profile are determined in real time in order for the summit height of the trajectory to be a desired value by deriving the summit height considering thrust performance, gravity, and other flight conditions. Computer simulation results demonstrate good performance of the proposed method.
Key Words: Initial Guidance, Thrust Vector Control, Pitch Command, Summit Height, Initial Trajectory
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