Synthesis of the augmented proportional navigation with lead bias aim point adapted to target for self-guided infrared missile
240 viewsDOI:
https://doi.org/10.54939/1859-1043.j.mst.77.2022.60-66Keywords:
Infrared self-guided surface to air missile; Augmented proportional navigation; Lead bias command aim point.Abstract
The paper presents the research results of augmented proportional navigation with taking into account a lead bias command aim point adapted to target for an infrared self-guided surface to air missile. The lead bias command in the terminal phase is proposed to engage the target kill probability. Simulation studies have demonstrated outstanding advantages of the proposed guidance law is compared with pure proportional navigation guidance.
References
[1]. Lê Anh Dũng, Nguyễn Hữu Độ, Nguyễn Xuân Căn, Huỳnh Lương Nghĩa, “Lý thuyết bay và hệ thống điều khiển tên lửa phòng không.” Học viện Kỹ thuật Quân sự, 1999.
[2]. Tô Văn Dực, “Hệ thống xử lý tín hiệu tên lửa tự dẫn hồng ngoại.” NXB Quân đội nhân dân, 2003, 263 tr.
[3]. Zarchan Paul, “Tactical and strategic missile guidance.” American Institute of Aeronautics and Astronautics, Inc., 2012.
[4]. Shneydor Neryahu A., “Missile guidance and pursuit: kinematics, dynamics and control.” Elsevier, 1998.
[5]. Hepner S.R., Geering H. P., “Observability Analysis for Target Maneuver Estimation Via Bearing-Only and Bearing-Rate-Only Measurements.” Journal of Guidance, Control, and Dynamics, Vol. 13, No. 6, 1990, pp. 977-983.
[6]. Song Taek Lyul, Tae Yoon Um, "Practical guidance for homing missiles with bearings-only measurements." IEEE Transactions on Aerospace and Electronic Systems, 32.1, 1996, pp. 434-443.
[7]. Đoàn Văn Thúy, Trần Hữu Phương, Phan Tương Lai, "Ứng dụng bộ lọc Kalman mở rộng trong bài toán điều khiển tên lửa tự dẫn bám sát mục tiêu." Tạp chí Nghiên cứu KH&CN Quân sự, Số đặc san FEE2020 (2020), tr. 66-73.
[8]. Singer R. A., “Estimating optimal tracking performance for manned maneuvering targets.” IEEE Transactions on Aerospace and Electronic Systems, 1970, pp. 473-483.
[9]. Техническая документация на изделие 9М39, Переносной зенитный ракетный комплекс 9К38, Технические условия на ракету 9М39, Часть 3.
