Journal of Institute of Control, Robotics and Systems (제어로봇시스템학회논문지)

Institute of Control, Robotics and Systems (제어로봇시스템학회)
권호 표지
DOI QR코드

DOI QR Code

Mixed Control of Agile Missile with Aerodynamic Fin and Thrust Vectoring Control

유도탄의 유도명령 추종을 위한 혼합제어기 설계 : 공력 및 추력벡터제어

  • Published : 2004.07.01
Download PDF
⟨ Previous Next ⟩

Abstract

This paper is concerned with a control allocation strategy using the dynamic inversion and the pseudo inverse control which generates the nominal control input trajectories. In addition, an autopilot design method is proposed by using time-varying control technique which is time-varying version of the pole placement of linear time-invariant system for an agile missile with aerodynamic fin and thrust vectoring control. The control allocation proposed in this paper is capable of extracting the maximum performance by combining each control effector, aerodynamic fin and thrust vectoring control. The adopted time-varying control technique for the autopilot design enhances the robustness of the tracking performance for a reference command. The main results are validated through the nonlinear simulations with aerodynamic data.

Keywords

References

  1. K. W. Wise, D. J. Broy, 'Agile Missile Dynamics and Control,' Journal of Guidance, Control, and Dynamics, vol. 21, No. 3, pp. 441-449, 1998 https://doi.org/10.2514/2.4256
  2. C. Song, Y.-S. Kim, 'Mixed Controlwith Aerodynamic Fin and Side Thruster Applied to Air Defense Missiles,' Proceedings of the International Conference on Control, Automation, and Systems, pp. 991-994, 2001
  3. R. F. Wilson, J. R. Cloutier, and R. K. Yedavalli, 'Control Design for Robust Eigenstructure Assignment in Linear uncertain Systems,' IEEE Control Systems Magazine, vol. 12, no. 5, pp. 29-34, 1992 https://doi.org/10.1109/37.158895
  4. R. T. Reichert, 'Dynamic Scheduling of Nodern-Robust-control Autopilot Designs for Missiles,' IEEE Control Systems Magazine, vol. 12, no. 5, pp. 35-42, 1992 https://doi.org/10.1109/37.158896
  5. J. S. Shamma, M. Athans, 'Gain-Scheduling: Potential Hazards and Possible Remedies,' IEEE Control Systems Magazine, vol. 12, no. 3, pp. 101-107, 1992 https://doi.org/10.1109/37.165527
  6. S. A. Snell, D. F. Enns, and W. L. Garrard, 'Nonlinear Inversion Flight Control for a Supermaneuverable Aircraft,' Journal of Guidance, Control and dynamics, vol. 15, no. 4, pp. 976-984, 1992 https://doi.org/10.2514/3.20932
  7. D. F. Enns, D. Bugajski, R. Hendrick, and G. Stein, 'Dynamic Inversion: An Evolving Methodology for Flight Control Design,' International Journal of Control, vol. 59, no. 1, pp. 71-91, 1994 https://doi.org/10.1080/00207179408923070
  8. J. Reiner, G. J. Balas, and W. L. Garrard, 'Robust Dynamic Inversion for Control of Highly Maneuverable Aircraft,' Journal of Guidance, Control and Dynamics, vol. 18, no. 1, pp. 18-24, 1995 https://doi.org/10.2514/3.56651
  9. D. Ito, J. Georgie, J. Valasek, and D. T. Ward, Re-Entry Vehicle Flight Controls Design Guidelines: Dynamic Inversion, NASA Technical Report, 2001
  10. J. J. Zhu, C. D. Johnson, 'Unified Canonical Forms for Matrices over a Differential Ring,' Linear Algebra and Its Application, vol. 147, pp. 201-248, 1991 https://doi.org/10.1016/0024-3795(91)90235-O
  11. J. J. Zhu, 이호철, 최재원, '선형 시변 시스템에 대한 잘 정의된 직렬 및 별렬 D-스팩트럼,' 제어 . 자동화 . 시스템공학 논문지, 제5권, 제5호, pp. 521-528, 1999
  12. J. W. Choi, H. C. Lee, and J. J. Zhu, 'Decoupling and Tracking Control Using Eigenstructure Assignment for Lineat Time-Varying Systems,' International Journal of Control, vol. 74, no. 5, pp. 453-464, 2001 https://doi.org/10.1080/00207170010008761
  13. 최재원, 이호철, '미분 Sylvester 방정식을 이용한 선형 시변 시스템의 고유구조 지정기법,' 제어 . 자동화 . 시스템공학 논문지, 제5권, 제7호, pp. 777-786, 1999
  14. 이호철, 최재원, '선형 시변 시스템의 고유치 지정을 위한 Ackermann형 공식,' 제어 . 자동화 . 시스템공학 논문지, 제9권, 제3호, pp. 186-195, 2003
  15. J. J. Zhu, M. C. Mickle, 'Missile Autopilot Design Using a New Linear Time-Varying Control Technique,' Journal of Guidance, Control and Dynamics, vol. 20, no. 1, pp. 150-157, 1997 https://doi.org/10.2514/2.4009
  16. 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 https://doi.org/10.1109/ACC.1998.688385