Abstract
The paper presents the results of research and propose synthesis methods of the remote control law when taking into the dynamics and nonlinear of the missile stage. Simple control law, capable of realization in practice. The simulation results show the advantages of control law in cases of target movement, small guidance error, ensuring good response to changing dynamic parameters of the missile during flight. Contribute to improving the quality of the missile control system, at the same time serving as a basis in the upgrade, improvement and new design of the flight device control system.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Van Bang, N.: Research and synthesize remote control loop of flying device using modern control technology. Technical doctoral thesis, Military Technical Academy, Viet Nam (2020)
Das, A., Das, R., Mukhopadhyay, S., Patra, A.: Robust nonlinear design of three axes missile autopilot via feedback linearization. In: Proceedings of the 27th IEEE Conference on Decision and Control, pp. 730–743 (2014)
Lee, C.-H., Lee, J.-I, Jun, B.-E.: Missile Acceleration Controller Design using PI and Time - Delay Adaptive Feedback Linearization Methodology. Agency for Defense Development (ADD), Daejeon, Korea (2001)
Lee, C.H., Kim, T.H., Tahk, M.J.: Missile autopilot design for agile turn using time delay control with nonlinear observer. Int. J. Aeronaut. Space Sci. Technol. 12(3), 266–273 (2011)
Devaud, E., Harcaut, J.P., Siguerdidjane, H.: Three-axes missile autopilot design: from linear to nonlinear control strategies. J. Guidance Control Dyn. 24(1), 64–71 (2001)
Bruyere, L., Tsourdos, A., White, B.A.: Robust augmented lateral acceleration flight control design for a quasi-linear parameter-varying missile. In: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 219 (2005)
Menon, P.K., Yousefpor, M.: Design of Nonlinear Autopilot for High Angle of Attack Missiles. In: AIAA Guidance, Navigation and Control Conference, pp. 3896–3913 (1996)
Menon, P.K., Iragavarapu, V.R., Ohlmeyer, E.J.: Nonlinear Missile Autopilot Using Time Scale Separation. AIAA Paper 96–3765 (1997)
Kim, S.H., Tahk, M.J.: Missile acceleration controller design using proportional-integral and non-linear dynamic control design method. In: Proceedings of Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 225 (2011)
Aнaтoлий Бopиcoвич Cкopик. “Cиcтeмы yпpaвлeния coвpeмeнными зeнитными paкeтaми. Maтeмaтичecкoe мoдeлиpoвaниe кoнтypa нaвeдeния”, Cyчacци инфopмaщйя тexнoлoги cфepe бeзпeки тa oбopoни (тoм 1) (2013)
Фeдocoв, E.A., Бoбpoнникoв, B.T., Кpacилыщикoв, M.H., Кyxтeнкo, B.И., Лeбeдeв, A.A., Maлыщeв, B.B., Opлoв, E.B., Пyчкoв, Б.B., Cилaeв, A.И., Cтeфaнoв, B.A.: Динaмичecкoe пpoeктиpoвaниe cиcтeм yпpaвлeния aвтoмaтичecкиx мaнeвpeнныx лeтaтeльныx aппapaтoв, Maшинocтpoeниe, Mocквa, cтp. 49–269 (1997)
Гoлyбeв И.C. и Cвeтлoв B.Г.: Пpoeктиpoвaниe зeнитныx yпpaвляeмыx paкeт, Издaтeльcтвo MAИ, Mocквa (2001)
Toлпeгин, O.A, Hoвикoв, B.Г.: Maтeмaтичecкиe мoдeлиcиcтeм нaвeдeния лeтaтeльныx aппapaтoв, Кoлoмнa, Издaтeльcтвo КИ (ф) MГOУ (2011)
Mизpoxи, B.Я.: Пpoeктиpoвaниe yпpaвлeния зeнитныx paкeт, Учeбнo-нayчнoe издaниe - M.: Изд., Экcлибpиc-Пpecc (2010)
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2021 The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.
About this paper
Cite this paper
Tuan, N.N., Thi, N.D., Van Bang, N., Van Tuyen, T. (2021). Synthesis of Remote Control Law When Taking into Dynamics and Nonlinear of the Missile Stage. In: Tran, DT., Jeon, G., Nguyen, T.D.L., Lu, J., Xuan, TD. (eds) Intelligent Systems and Networks . ICISN 2021. Lecture Notes in Networks and Systems, vol 243. Springer, Singapore. https://doi.org/10.1007/978-981-16-2094-2_22
Download citation
DOI: https://doi.org/10.1007/978-981-16-2094-2_22
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-16-2093-5
Online ISBN: 978-981-16-2094-2
eBook Packages: Intelligent Technologies and RoboticsIntelligent Technologies and Robotics (R0)