[1] Cottrell, R. G., "Optimal Intercept Guidance for Short-Range Tactical Missiles," AIAA Journal, Vol. 9, No. 7, pp. 1414-1415, 1971, doi: 10.2514/3.6369.
[2] Rusnak, I. and Meir, L., "Modern Guidance Law for High-Order Autopilot," Journal of Guidance, Control, and Dynamics, Vol. 14, No. 5, pp. 1056-1058, 1991.
[3] Rusnak, I. and Meir, L., "Optimal Guidance Law for Acceleration Constrained Missile and Maneuvering Target," IEEE Transactions on Aerospace and Electronic Systems, Vol. 26, No. 4, pp. 618-624, 1990.
[4] Blackburn, T. R., "Method for Improving Autopilot Lag Compensation in Intercept Guidance," Journal of Guidance, Control, and Dynamics, Vol. 19, No. 3, pp. 724-726, 1996, doi: 10.2514/3.21686.
[5] Jalali-Naini, S. H., "Modern Explicit Guidance Law for High-Order Dynamics," Journal of Guidance, Control, and Dynamics, Vol. 27, No. 5, pp. 918-922, 2004, doi: 10.2514/1.5902.
[6] Bryson, A. E. and Ho, Y. C., Applied Optimal Control. Hemisphere, New York, 1975.
[7] Zarchan, P., Tactical and Strategic Missile Guidance. American Institute of Aeronautics and Astronautics, Inc., 2012.
[8] Yanushevsky, R. T. and Boord, W. J., "New Approach To Guidance Law Design," Journal of Guidance, Control, and Dynamics, Vol. 28, No. 1, pp. 162-166, 2005, doi: 10.2514/1.6154.
[9] Jalali-Naini, S. H., "Miss Distance Analysis of Proportional Navigation Using Normalized Equations with Radome Effect, Saturation, and Body Rate Feedback," Journal of Aeronautical Engineering, Vol. 14, No. 1, pp. 1-11, 2012 (in Persian).
[10] Maklouf, O., Basha, S. and Eljubrani, A., "Performance Evaluation of Proportional Navigation Homing Guidance Law," in 5th International Conference on Control Engineering & Information Technology, 2017, Vol. 33, pp. 14-18.
[11] Yanushevsky, R., Modern Missile Guidance. Taylor & Francis, 2007.
[12] Chauhan, D. S. and Sharma, R., "A Computing Based Simulation Model for Missile Guidance in Planar Domain," Journal of The Institution of Engineers (India): Series C, Vol. 99, No. 6, pp. 607-628, 2018, doi: 10.1007/s40032-017-0386-6.
[13] Alpert, J., "Normalized Analysis of Interceptor Missiles Using the Four-State Optimal Guidance System," Journal of Guidance, Control, and Dynamics, Vol. 26, No. 6, pp. 838-845, 2003, doi: 10.2514/2.6927.
[14] Bucco, D., Zarchan, P. and Weiss, M., "On Some Issues Concerning the Adjoint Simulation of Guidance Systems," in AIAA Guidance, Navigation, and Control Conference, 2012.
[15] Balakrishnan, S. N., Tsourdos, A. and White, B. A., Advances in Missile Guidance, Control, and Estimation. CRC Press, 2016.
[16] He, T., Chen, W., "A New Interpretation of Adjoint Method in Linear Time-Varying System Analysis," presented at the 2017 IEEE International Conference on Cybernetics and Intelligent Systems (CIS) and IEEE Conference on Robotics, Automation and Mechatronics (RAM), pp. 58-63, 2017.
[17] Alpert, J., "Adjoint Analysis of Guidance Systems for Time-Series Inputs Using Fourier Analysis," Journal of Guidance, Control, and Dynamics, Vol. 43, No. 7, pp. 1359-1364, 2020, doi: 10.2514/1.G005166.
[18] Jalali-Naini, S. H., "Noise-Induced Miss Distance Formulas of First-Order Control System Under Proportional Navigation for Arbitrary Navigation Ratios," presented at the 15th International Conference of Iranian Aerospace Society, Civil Aviation Technology College, Tehran, Iran, 2016.
[19] Jalali-Naini, S. H., "Noise-Induced Miss Distance Analysis of Proportional Navigation with Acceleration Feedback for Second-Order System Using Normalized Adjoint Method," Journal of Aeronautical Engineering, Vol. 15, No. 2, pp. 59-73, 2014.
[20] Jalali-Naini, S. H. and Arabian Arani, A., "Miss Distance Analysis of Proportional Navigation for High-Order Binomial Control Systems in Presence of Noise and Target Maneuvers," Journal of Aeronautical Engineering, Vol. 18, No. 1, pp. 34-50, 2016 (in Persian).
[21] Arabian Arani, A. and Jalali-Naini, S. H., "Approximate Miss Distance Formulas of Proportional Navigation Due to Time Delay Based on Worst Case Analysis," Aerospace Knowledge and Technology Journal, Vol. 7, No. 1, pp. 47-62, 2018 (in Persian).
[22] Jalali-Naini, S. H., "Generalized Explicit Guidance Law for Time-Variant High-Order Dynamics," in Proceedings of the 4th Iranian Aerospace Society Conference, Iranian Aerospace Society, Tehran, Iran, 2003, pp. 249-261.
[23] Jalali-Naini, S. H. and Arabian Arani, A., "Explicit Guidance Law with Variable Navigation Coefficient," Presented at the 29th Annual International Conference of the Iranian Association of Mechanical Engineers, Tehran, Iran, 2021 (in Persian).