Missile Autopilot Design for Agile Turn Control During Boost-Phase |
Ryu, Sun-Mee
(Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology)
Won, Dae-Yeon (Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology) Lee, Chang-Hun (Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology) Tahk, Min-Jea (Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology) |
1 | Wise, K. A. and Broy, D. J. (1998). Agile missile dynamics and control. Journal of Guidance, Control, and Dynamics, 21, 441-449. DOI ScienceOn |
2 | Zarchan, P. (2007). Tactical and Strategic Missile Guidance, 5th ed. Progress in Astronautics and Aeronautics, Vol. 219. Reston: American Institute of Aeronautics and Astronautics. |
3 | Zipfel, P. H. (2000). Modeling and Simulation of Aerospace Vehicle Dynamics. Reston: American Institute of Aeronautics and Astronautics. |
4 | Innocenti, M. (2001). Nonlinear guidance techniques for agile missiles. Control Engineering Practice, 9, 1131-1144. DOI ScienceOn |
5 | Lawrence, D. A. and Rugh, W. J. (1993). Gain scheduling dynamic linear controllers for a nonlinear plant. Proceedings of the 32nd IEEE Conference on Decision and Control, San Antonio, TX. pp. 1024-1029. |
6 | Lee, C. H., Kim, T. H., and Tahk, M. J. (2009). Design of missile autopilot for agile turn using nonlinear control. Proceeding of the Korean Socieyt for Aeronautical & Space Sciences Conference, Korea. pp. 667-670. |
7 | Mehrabian, A. R. and Roshanian, J. (2006). Design of gainscheduled autopilot for a highly-agile missile. Proceedings of the 1st International Symposium on Systems and Control in Aerospace and Astronautics, Harbin, China. pp. 144-149 |
8 | Menon, P. K. and Yousefpor, M. (1996). Design on nonlinear autopilots for high angle of attack missiles. Proceedings of the AIAA Guidance, Navigation, and Control Conference, San Diego, CA. pp. 29-31. |
9 | Thukral, A. and Innocenti, M. (1998). A sliding mode missile pitch autopilot synthesis for high angle of attack maneuvering. IEEE Transactions on Control Systems Technology, 6, 359-371. DOI ScienceOn |
10 | White, D. P., Wozniak, J. G., and Lawrence, D. A. (1994). Missile autopilot design using a gain scheduling technique. Proceedings of the 26th Southeastern Symposium on System Theory, Athens, OH. pp. 606-610. |