Nonlinear Suboptimal Guidance Law with Impact Angle Constraint: An SDRE-Based Approach

Chunyan Wang, Wei Dong, Jianan Wang*, Jiayuan Shan

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

40 Citations (Scopus)

Abstract

In this article, a guidance law with impact angle constraint is developed using the state-dependent Riccati equation (SDRE) technique. First, the nonlinear guidance dynamics consisting of line-of-sight (LOS) angle rate and error is formulated under a planar engagement scenario. After the state-dependent coefficient parameterization, a nonlinear regulator problem is formed to concurrently zero LOS angle rate and error. Second, a preliminary guidance law is directly developed under the framework of the SDRE technique. By applying the Lyapunov stability analysis, a nonlinear suboptimal guidance law is obtained through further parameter modifications. Then, the proposed guidance law is extended to attack maneuvering targets. Finally, the effectiveness of the proposed guidance law is demonstrated through numerical simulations.

Original languageEnglish
Article number9121735
Pages (from-to)4831-4840
Number of pages10
JournalIEEE Transactions on Aerospace and Electronic Systems
Volume56
Issue number6
DOIs
Publication statusPublished - Dec 2020

Keywords

  • Guidance law
  • SDC
  • SDRE
  • impact angle constraint
  • maneuvering target
  • nonlinear optimal control

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