JERAJournal of Electronic Research and Application2208-35022208-3510Bio-Byword Scientific Publishing Pty. Ltd.10.26689/jera.v8i5.8400ArticleDesign and Analysis of Terminal Guidance Law for Kinetic Interceptors based on Pulse Engine https://artdesignp.com/journal/JERA/8/5/10.26689/jera.v8i5.8400LiShixin,MaJia,YueShuai2024852024-09-30A new terminal guidance law is proposed based on a solid propellant pulse engine and an improved proportional navigation method to address the terminal guidance issue for kinetic interceptors. On this basis, the start-stop curve of the pulse motor during the terminal guidance process is designed, along with its start-up logic. The effectiveness of the proposed guidance strategy is verified through simulation.

Zhan X, Han P, Chen P, 2013, Design of Terminal Guidance Law for Kinetic Interceptors based on Nonlinear Terminal Sliding Mode. Journal of Northwestern Polytechnical University, 31(2): 233–238.

Erer KS, Merttopcuoglu O, 2012, Indirect Impact-Angle-Control Against Stationary Targets using Biased Pure Proportional Navigation. Journal of Guidance, Control, and Dynamics, 35(2): 700–703. https://doi.org/10.2514/1.52105

Lee CH, Kim TH, Tahk MJ, 2013, Interception Angle Control Guidance using Proportional Navigation with Error Feedback. Journal of Guidance, Control, and Dynamics, 36(5): 1556–1561.

Lu P, Doman DB, Schierman JD, 2006, Adaptive Terminal Guidance for Hypervelocity Impact in Specified Direction. Journal of Guidance, Control, and Dynamics, 29(2): 269–278.

Ratnoo A, Ghose D, 2008, Impact Angle Constrained Interception of Stationary Targets. Journal of Guidance, Control, and Dynamics, 31(6): 1816–1821.

Tian H, Liang X, Jia X, 2011, Target Observability Criteria from Bearing-Rate-Only Measurements. Journal of Beijing University of Aeronautics and Astronautics, 37(5): 534–537.

Tian H, Liang X, Jia X, 2012, Research of Effect of Line-of-Sight Rate Measurement Disturb on Navigation System. Journal of Ballistics, 24(3): 65–69.

Zhang YA, Ma GX, Lu AL, 2013, Guidance Law with Impact Time and Impact Angle Constraints. Chinese Journal of Aeronautics, 26(4): 960–966.

Huang J, Zhang Y, Liu Y, 2016, A Biased Proportional Guidance Algorithm for Moving Target with Impact Angle and Field-of-View Constraints. Journal of Astronautics, 37(2): 195–202.

Gu J, Chen W, 2013, Homing Guidance with Look Angle and Impact Angle Constraints. Journal of Astronautics, 34(6): 782–787.

Yan L, Zhao J, Li Y, 2015, Guidance Law with Angular Constraints for Head-Pursuit or Head-on Engagement. Journal of Beijing University of Aeronautics and Astronautics, 41(5): 857–862.

Li Y, Zhao J, Yan L, et al., 2015, Biased Proportional Navigation Guidance Law for Maneuvering Targets Interception with Angular Constraints. Journal of Equipment Academy, 26(5): 71–76.

Turgut ET, Rosen MA, 2012, Relationship between Fuel Consumption and Altitude for Commercial Aircraft during Descent: Preliminary Assessment with a Genetic Algorithm. Aerospace Science and Technology, 17(1): 65–73.

Baklacioglu T, 2016, Modeling the Fuel Flow Rate of Transport Aircraft during Flight Phases using Genetic Algorithm-Optimized Neural Networks. Aerospace Science and Technology, 49: 526–536.

Zhang HF, Wang XH, Chen XF, 2015, Support Vector with ROC Optimization Method based Fuel Consumption Modeling for Civil Aircraft. Procedia Engineering, 99: 296–303.

Zheng LW, Jing WX, Gu LX, 2007, A Terminal Guidance Law For Exoatmospheric Kill Vehicle. Acta Aeronautica et Astronautica Sinica, 28(4): 953–958.

Zhu B, Quan Q, Cai KY, 2007, BP Networks Method of Handover Point of KKV. Journal of Beijing University of Aeronautics and Astronautics, 33(3): 332–335.