Mixed Control of Agile Missile with Aerodynamic Fin and Thrust Vectoring Control
![]() |
이호철
(부산대학교 기계공학부 대학원)
최용석 (부산대학교 기계공학부 대학원) 최재원 (부산대학교 기계공학부 및 기계기술연구소) 송택렬 (한양대학교 전자ㆍ컴퓨터공학부) 송찬호 (국방과학연구소) |
1 | K. W. Wise, D. J. Broy, 1998, 'Agile Missile Dynamics and Control,' Journal of Guidance, Control, and Dynamics, Vol.21, No.3, pp.441-449 DOI ScienceOn |
2 | C. Song, Y.-S. Kim, 2001, 'Mixed Control with Aerodynamic Fin and Side Thruster Applied to Air Defense Missiles,' Proceedings of the International Conference on Control, Automation, and Systems, pp.991-994 |
3 | J. J. Zhu, M. C. Mickle, 'Synthesis of Time-Varying Bandwidth Filters Based on All-Pole Prototypes,' Proceedings of the 1998 American Control Conference, pp.2889-2894, 1998 |
4 | J. J. Zhu, M. C. Mickle, 1997, 'Missile Autopilot Design Using a New Linear Time-Varying Control Technique,' Journal of Guidance, Control and Dynamics, Vol.20, No.1, pp.150-157 DOI ScienceOn |
5 | S. A. Snell, D. F. Enns, and W. L. Garrard, 1992, 'Nonlinear Inversion Flight Control for a Supermaneuverable Aircraft,' Journal of Guidance, Control and Dynamics, Vol.15, No.4, pp.976-984 DOI |
6 | L. M. Silverman, 1996, 'Transformation of Time-Variable Systems to Canonical (Phase-Variable) Form,' IEEE Transactions on Automatic Control, Vol.11, No.2, pp.300-303 |
![]() |