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相 对 距 离 剖 面 高 阶 重 塑 的 多 约 束 末 制 导 律

Translated title of the contribution: Terminal guidance law under multiple constraints of high-order reshaping of relative range profile
  • Beihang University

Research output: Contribution to journalArticlepeer-review

Abstract

To address the problem of homing guidance with impact angle constraint or impact time constraint under the condition of limited field-of-view of missile’s seeker,a multi-constraint homing guidance law design method based on high-order reshaping of relative range profile is proposed. Firstly,an auxiliary variable containing only field-of-view angle is constructed for the two-dimensional plane homing guidance model,and a high-order polynomial with the refer- ence missile-target relative range profile as the auxiliary variable is designed. Secondly,some profile parameters are solved by using the initial and terminal boundary conditions of guidance,and the expression forms of the parameters to be solved are given by performing terminal constraint integration on the auxiliary variable transformation equation. Fur- thermore,the impact angle constrained guidance law and impact time constrained guidance law driven by reference profile are given based on model transformation. At the same time,to ensure continuous attenuation of the seeker’s field-of-view,the conditions for the profile parameters to be satisfied are given. On this basis,the explicit representa- tion form of the available sets of angle constraint and time constraint are derived. Different from the existing guidance law with profile reshaping,this paper designs a general n-order range profile reshaping guidance method,which can obtain wider achievable constraint sets,and is also convenient for designers/engineers to analyze the reshaping guid- ance law performance under arbitrary orders. In addition,to solve the profile deviation problem in the ideal profile re- shaping process under uncertainty or disturbance,the guidance law is compensated for profile tracking deviation and is robustly corrected,thereby improving the multi-constraint guidance accuracy under complex working conditions. Fi- nally,the effectiveness and robustness of the designed guidance law are verified through numerical simulation com- parison analysis under various working conditions and Monte Carlo tests.

Translated title of the contributionTerminal guidance law under multiple constraints of high-order reshaping of relative range profile
Original languageChinese (Traditional)
Article number531405
JournalHangkong Xuebao/Acta Aeronautica et Astronautica Sinica
Volume46
Issue number6
DOIs
StatePublished - 25 Mar 2025

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