References
- Escande, B., "Nonlinear Dynamic Inversion and Linear Quadratic Techniques", AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA, pp.1998-4245, 1998
- 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
- 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
- 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
- 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
- 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 https://doi.org/10.1109/87.238400
- Reichert, R. "Dynamic Scheduling of Modem Robust Control Autopilot Designs for Missiles", IEEE Control Systems Magazine, Vol. 12, No. 5, pp.35-42, 1992
- 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
- 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 https://doi.org/10.2514/2.4266
- 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 https://doi.org/10.2514/3.20997
- 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 https://doi.org/10.2514/3.20932
- 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
- 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