A study on control command synthesis algorithm for single-channel flying equipment with linear steering vane
107 viewsDOI:
https://doi.org/10.54939/1859-1043.j.mst.106.2025.28-39Keywords:
Single-channel flying equipment; Command control; Linear steering machine; Algorithm.Abstract
This paper presents the algorithm and mathematical foundation for control command synthesis applied to single-channel flying equipment equipped with a linear steering vane. The proposed algorithm is developed based on optimal control principles, with a cost function aiming to minimize control energy. From the resulting control law, a relationship is established between the control signal and the normal force acting on the flying equipment. Simulation results are conducted to demonstrate the superiority of the proposed control law over relay-based control, particularly in applications involving single-channel flying equipment.
References
[1]. В.М. Кашим, А.Л. Лифиц: “Основы проектирования переносных зенитных ракетных комплексов”. Гродно ГрГУ им. Я. Купалы, Москва, (2014).
[2]. Nguyen Van Son. “Regarding the control problem of single-channel guided flying equipment”, Technical PhD thesis, Academy of Military Science and Technology, (2007).
[3]. Phan Van Tu. “Construct method and control algorithms for the class Single-channel flying
equipment”, Technical PhD thesis, Academy of Military Science and Technology, (2010).
[4]. Nguyen Duc Cuong, Tran Duc Thuan. “Guided flying equipment and anti-ship cruise missiles”, People's Army Publishing House, (2015).
[5]. To Ba Thanh. “Researching on synthesizing of guiding and steering control algorithm for a class of two-channel aerial vehicle rotating around the longitudinal axis”, Technical PhD thesis, Academy of Military Science and Technology, (2024).
[6]. Казаков И .Е, Мишаков А Φ: “Авиационые управляемые ракеты”, BВИА им проф. Н.Е. Жуковского, (1988).
[7]. Пугачёв В. С: “Основы автоматического управления”, Наука Мосва, (1974).
[8]. Q. F. Gao et al., “Autopilot design of single channel rolling missile”. Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology, (2011).
[9]. E.C. Suiçmez, A.T. Kutay. “Single channel digital controller design for a high spinningrate rolling airframe missile”. Aeronautical Journal -New Series- 126(1305), (2022). DOI: https://doi.org/10.1017/aer.2022.30
[10]. T.-V. Chelaru, Valentin Pana, Cristian Emil Constantinescu, Costin Ene, Chelaru Adrian: “Stability of Single-Channel Homing Rolling Aerospace Vehicle”. Aerospace ISSN: 2226-4310, (2024). DOI: https://doi.org/10.20944/preprints202405.1816.v1
