Approximate Optimum of Airplane Engagement Maneuvering Strategy with Allowable Deviation
ZHAO Yu
ZHANG Bin
SUI Yong-hua
XU An
Abstract：The controllers fluctuate wildly because of the fighter maneuvering in air combat engagement process,which has effect on fighter’s performance and pilot’s controlling.According to the optimal prob-lem of guidance strategy,an approximate optimum of engagement maneuvering strategy with allowable deviation is proposed.Firstly,three degree of freedom motion model is built.At the same time,the solu-tion steps of angle deviation are put forward.Secondly,the discrete nonlinear programming model is built and the restriction and obj ective function are analyzed.After that,it introduces receding horizon control and proposes a numerical solution of controlling process.At last,an example of forward hemisphere attack is designed to comparing proportional navigation strategy with the designed engagement maneuvering strategy.The result shows that the latter’s controllers fluctuate more smoothly.Therefore,It is an effec-tive strategy which can lighter pilot’s operation pressure.
Keywords：engagement maneuvering strategyreceding horizon controlallowable deviationcontrolled variable
Publication Date：2015-01-01
Online Publishing Date：2025-08-15(First online date of this platform, not the publication date of the document)
Pages：5( 19-23 )