Browse > Article

Robust Missile Autopilot Design using Dynamic Inversion and PI Control  

Cho, Sung-Jin (ADD)
Publication Information
Journal of the Korea Institute of Military Science and Technology / v.10, no.2, 2007 , pp. 53-60 More about this Journal
Abstract
This paper presents a robust nonlinear autopilot design method based on dynamic inversion and PI(Proportional-Integral) control law. The new controller structure which is different from previous work is composed of classical linear PI control law and nonlinear fast dynamic inversion. A pitch axis model of highly maneuverable missiles and a linearized model for designing Pl controller are presented. The performance of proposed method is illustrated via nonlinear simulations including aerodynamic uncertainties and actuator dynamics.
Keywords
Missiles; Flight Control; Nonlinear Control; Dynamic Inversion; Robustness;
Citations & Related Records
연도 인용수 순위
  • Reference
1 Escande, B., "Nonlinear Dynamic Inversion and Linear Quadratic Techniques", AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA, pp.1998-4245, 1998
2 McFarland, M. B. and S. M. Hoque, "Robustness of a Nonlinear Missile Autopilot Designed using Dynamic Inversion", AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA, pp.2000 - 3970, 2000
3 Schumacher C. and P. P. Khargonekar, "Stability Analysis of a Missile Control System with a Dynamic Inversion Controller", Journal of Guidance, Control, and Dynamics, Vol. 21, No.3, pp.508-515, 1998   DOI   ScienceOn
4 Shamma, J. S. and J. R. Cloutier, "Gain Scheduled Missile Autopilot Design Using Linear Parameter Varying Transformation", Journal of Guidance, Control, and Dynamics, Vol. 16, No.2, pp.256-263, 1993   DOI   ScienceOn
5 Nichols, R. A., R. T. Reichert and W. J. Rugh, "Gain Scheduling for H Infinity Controllers : A Flight Control Example", IEEE Trans. On Control Systems Technology, Vol. 1, No.2, PP.69-79, 1993   DOI
6 McFarland, M. B. and C. N. D'Souza, "Missile Autopilot Design using Dynamic Inversion and Structured Singular Value Synthesis", Proc. of the American Control Conference, pp.959-961, 1994
7 Menon, P. K., V. R. Iragavarapu and E. J. Ohlmeyer, "Nonlinear Missile Autopilot Design using Time Scale Separation", AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA, pp.1997-3765, 1997
8 Snell, S., A., 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   DOI
9 Steinberg, M. L., "A Comparion of Intelligent, Adaptive, and Nonlinear Flight Control Laws", AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA, pp. 1999-4044, 1999
10 Reichert, R. "Dynamic Scheduling of Modem Robust Control Autopilot Designs for Missiles", IEEE Control Systems Magazine, Vol. 12, No. 5, pp.35-42, 1992
11 Steinicke, A. and G. Michalka, "Improving Transient Performance of Dynamic Inversion Missile Autopilot by Use of Backstepping", AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA, pp.2002-4658, 2002
12 Schumacher C. and P. P. Khargonekar, "A Comparison of Missle Autopilot Design using HInfinity Control with Gain Scheduling and Nonlinear Dynamic Inversion", Proc. of the American Control Conference, pp.2759 - 2763, 1997
13 Hull, R. A. and Z. Qu, "Dynamic Robust Recursive Control Design and Its Application to a Nonlinear Missile Autopilot", Proc. of the American Control Conference, pp.833-837, 1997