[1] Zarchan P. Tactical and strategic missile guidance: American Institute of Aeronautics and Astronautics, Inc.; 2012##.
[2] Palumbo NF, Blauwkamp RA, Lloyd JM. Basic principles of homing guidance. Johns Hopkins APL Technical Digest. 2010;29(1):25-41##.
[3] Lin C-F, Bibel J, Ohlmeyer E, Malyevac S, editors. Optimal design of integrated missile guidance and control. AIAA and SAE, 1998 World Aviation Conference; 2007##.
[4] Cloutier JR, D’Souza CN, Mracek CP, editors. Nonlinear regulation and nonlinear H∞ control via the state-dependent Riccati equation technique: Part 1, theory. Proceedings of the international conference on nonlinear problems in aviation and aerospace; 1996: Embry Riddle University##.
[5] Cloutier JR. Adaptive matched augmented proportional navigation. Google Patents; 2001##.
[6] Mracek CP, Cloutier JR, editors. Missile longitudinal autopilot design using the state-dependent Riccati equation method. Proceedings of the International Conference on Nonlinear Problems in Aviation and Aerospace; 1996##.
[7] Menon P, Ohlmeyer EJ. Integrated design of agile missile guidance and autopilot systems. Control Engineering Practice. 2001;9(10):1095-106##.
[8] Palumbo NF, Jackson TD, editors. Integrated missile guidance and control: A state dependent Riccati differential equation approach. Proceedings of the 1999 IEEE International Conference on Control Applications (Cat No 99CH36328); 1999: IEEE##.
[9] Menon P, Sweriduk G, Ohlmeyer EJ, Malyevac D. Integrated guidance and control of moving-mass actuated kinetic warheads. Journal of Guidance, control, and Dynamics. 2004;27(1):118-26##.
[10] Menon P, Vaddi S, Ohlmeyer E, editors. Finite-horizon robust integrated guidance-control of a moving-mass actuated kinetic warhead. AIAA guidance, navigation, and control conference and exhibit; 2006##.
[11] Hwang T-W, Tahk M-J, editors. Integrated backstepping design of missile guidance and control with robust disturbance observer. 2006 SICE-ICASE International Joint Conference; 2006: IEEE##.
[12] Harl N, Balakrishnan S, Phillips C, editors. Sliding mode integrated missile guidance and control. AIAA guidance, navigation, and control conference; 2010##.
[13] Harl N, Balakrishnan S. Reentry terminal guidance through sliding mode control. Journal of guidance, control, and dynamics. 2010;33(1):186-99##.
[14] Wang XH, Tan CP, Cheng LP. Impact time and angle constrained integrated guidance and control with application to salvo attack. Asian Journal of Control. 2020;22(3):1211-20##.
[15] He S, Song T, Lin D. Impact angle constrained integrated guidance and control for maneuvering target interception. Journal of Guidance, Control, and Dynamics. 2017;40(10):2653-61##.
[16] Ma J, Guo H, Li P, Geng L. Adaptive Integrated Guidance and Control Design for a Missile With Input Constraints. IFAC Proceedings Volumes. 2013;46(20):206-11##.
[17] Cross M. Missile Interceptor Integrated Guidance and Control: Single-Loop Higher-Order Sliding Mode Approach: The University of Alabama in Huntsville; 2020##.
[18] Lee KW, Singh SN. Longitudinal nonlinear adaptive autopilot design for missiles with control constraint. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 2018;232(9):1655-70##.
[19] Ma M, Zhao K, Song S. Adaptive sliding mode guidance law with prescribed performance for intercepting maneuvering target. Int J Innov Comput, Inform Control. 2020;16(2):631-48##.
[20] Mingzhe H, Guangren D. Integrated guidance and control of homing missiles against ground fixed targets. Chinese Journal of aeronautics. 2008;21(2):162-8##.
[21] Cross MA, Shtessel YB. Single-loop integrated guidance and control using high-order sliding-mode control. Variable-Structure Systems and Sliding-Mode Control: From Theory to Practice. 2020:433-62##.
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