[1] Gagnon E, Lauzon M. Low cost guidance and control solution for in-service unguided 155 mm artillery shell. Defence Research and Development Canada, DRDC-VALCARTIER-TR-2008-333. 2009.
[2] Reusch O, Kautzsch K, editors. Precision enhancement build on a multi functional fuze for 155mm artillery munition. Proceedings of the 47th NDIA Annual Fuze Conference (NDIA’03); 2003.
[3] Beattie R, editor UK Course Correction Fuze Research. 6th International Cannon Artillery Firepower Symposium & Exhibition; 2000.
[4] D'Amico W. Low-cost Competent Munitions (LCCM) Self-Correction Devices-An Initial Study and Status. US Army Research Laboratoiy, Aberdeen Proving Ground, MD, ARL-TR-1. 1996;178.
[5] Eroğlu M. Design and control of nose actuation kit for position correction of spin stabilized munitions under wind effect: Middle East Technical University; 2016.
[6] Fresconi F, Celmins I, Silton S, Costello M. High maneuverability projectile flight using low cost components. Aerospace Science and Technology. 2015;41:175-88.
[7] Theodoulis S, Gassmann V, Wernert P, Dritsas L, Kitsios I, Tzes A. Guidance and control design for a class of spin-stabilized fin-controlled projectiles. Journal of Guidance, Control, and Dynamics. 2013;36(2):517-31.
[8] Nobahari H, Arab Kermani M. Integrated Optimization of Guidance and Control Parameters in a Dual Spin Flying Vehicle. Scientia Iranica. 2017;24(5):2473-89.
[9] Zhu D, Tang S, Guo J, Chen R. Flight stability of a dual-spin projectile with canards. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 2015;229(4):703-16.
[10] Wernert P, Theodoulis S, Morel Y, editors. Flight dynamics properties of 155 mm spin-stabilized projectiles analyzed in different body frames. AIAA atmospheric flight mechanics conference; 2010.
[11] Wernert P, Theodoulis S, editors. Modelling and stability analysis for a class of 155 mm spin-stabilized projectiles with course correction fuse (CCF). AIAA atmospheric flight mechanics conference; 2011.
[12] Spagni J, Theodoulis S, Wernert P, editors. Flight control for a class of 155 mm spin-stabilized projectile with reciprocating canards. AIAA Guidance, Navigation, and Control Conference; 2012.
[13] Seve F, Theodoulis S, Wernert P, Zasadzinski M, Boutayeb M. Flight dynamics modeling of dual-spin guided projectiles. IEEE Transactions on Aerospace and Electronic Systems. 2017;53(4):1625-41.
[14] Costello M, editor Modeling and simulation of a differential roll projectile. AIAA Modeling and Simulation Technologies Conference and Exhibit; 1998.
[15] Theodoulis S, Sève F, Wernert P. Robust gain-scheduled autopilot design for spin-stabilized projectiles with a course-correction fuze. Aerospace Science and Technology. 2015;42:477-89.
[16] Zheng Q, Zhou Z. Flight Stability of Canard-Guided Dual-Spin Projectiles with Angular Rate Loops. International Journal of Aerospace Engineering. 2020;2020.
[17] Wernert P, editor Stability analysis for canard guided dual-spin stabilized projectiles. AIAA atmospheric flight mechanics conference; 2009.
[18] Wang Y, Wang X-m, Yu J-y. Influence of control strategy on stability of dual-spin projectiles with fixed canards. Defence technology. 2018;14(6):709-19.
[19] Norris J, Hameed A, Economou J, Parker S. A review of dual-spin projectile stability. Defence Technology. 2020;16(1):1-9.
[20] Zhang X, Xiaoxian Y, Zheng Q. Impact point prediction guidance based on iterative process for dual-spin projectile with fixed canards. Chinese Journal of Aeronautics. 2019;32(8):1967-81.
[21] Zhang Y, Gao M, Yang S, Fang D. An adaptive proportional navigation guidance law for guided mortar projectiles. The Journal of Defense Modeling and Simulation. 2016;13(4):467-75.
[22] Guo Q-w, Song W-d, Wang Y, Lu Z-c. Guidance law design for a class of dual-spin mortars. International Journal of Aerospace Engineering. 2015;2015.
[23] Liu P, Cao H, Feng S, Liu H, Cao L. Optimization of the PNG Law for a Dual-Spin Mortar with Fixed Canards. Mathematical Problems in Engineering. 2021;2021.
[24] Yuan P-J, Chern J-S. Ideal proportional navigation. Journal of Guidance, Control, and Dynamics. 1992;15(5):1161-5.