Abstract
A novel global sliding mode control (GSMC) based guidance method is proposed for intercepting target with impact angle constraint. In this paper, we take advantage of a new guidance concept, which enables the system to intercept a maneuvering target while can also imposes a predefined intercept angle. By designing GSMC surface, our method cancels the reaching phase so that the system is robust to parameter uncertainties. What’s more, the system state converges to origin at an exponential rate. To compensate the effect of disturbance, an observer with fast convergence property is utilized. Numerical simulations are performed to validate the performance of the designed guidance strategy.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Similar content being viewed by others
References
Ming, X., Balakrishnan, S.N.: A new optimal nonlinear control method and its application to missile guidance law design. In: AIAA Guidance, Navigation, and Control Conference and Exhibit, Monterey, USA (2002)
Gao, C., Jing, W., Li, C.: Optimal guidance law design for re-entry vehicle using virtual displacement concept. In: Chinese Control Conference, pp. 507–510, Hunan, China (2007)
Lee, Y.I., Kim, S.H., Tahk, M.J.: Optimality of linear time-varying guidance for impact angle control. IEEE Trans. Aerosp. Electron. Syst. 48(4), 2802–2817 (2012)
Tao, C., Wang, S., Ming, Y.: Angular constrained guidance law and its optimization with hybrid optimization algorithm. In: Guidance, Navigation and Control Conference, pp. 2455–246, Yantai, China (2015)
Xie, D.C., Wang, Z.W.: Optimal guidance law design for re-entry vehicles with terminal velocity and angle constraints. Adv. Mater. Res. 459(5), 505–509 (2012)
Zhang, Q., Wang, Z., Tao, F.: Optimal guidance law design for impact with terminal angle of attack constraint. Optik 125(1), 243–251 (2014)
Dou, L., Dou, J.: The design of optimal guidance law with multi-constraints using block pulse functions. Aerosp. Sci. Technol. 23(1), 201–205 (2012)
Lee, C.H., Shin, H.S., Tsourdos, A.: A new command shaping guidance law using Lagrange multiplier. IFAC PapersOnLine 50(1), 15185–15190 (2017)
Liu, D.W., Xia, Q., Du, Y.: Miss distance and impact angle error of trajectory shaping guidance law based on statistical linearization adjoin method. Energy Proc. 11(13), 6370–6377 (2011)
Erer, K.S.: Indirect impact-angle-control against stationary targets using biased pure proportional navigation. J. Guid. Control Dyn. 35(2), 700–704 (2012)
Shima, T.: Intercept-Angle Guidance. J. Guid. Control Dyn. 34(2), 484–492 (2012)
Levant, A.: High-order sliding modes, differentiation and output feedback control. Int. J. Control 76(9), 924–941 (2003)
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2022 The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.
About this paper
Cite this paper
Zhang, W., Yi, W. (2022). Observer-Based Global Sliding Mode Impact Angle Control Guidance Law. In: Yan, L., Duan, H., Yu, X. (eds) Advances in Guidance, Navigation and Control . Lecture Notes in Electrical Engineering, vol 644. Springer, Singapore. https://doi.org/10.1007/978-981-15-8155-7_51
Download citation
DOI: https://doi.org/10.1007/978-981-15-8155-7_51
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-15-8154-0
Online ISBN: 978-981-15-8155-7
eBook Packages: Intelligent Technologies and RoboticsIntelligent Technologies and Robotics (R0)