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Integrated Guidance and Control Design based on a Reference Model
Jian Chen,Qingdong Li,Cunjia Liu,Peng Li,Zhang Ren 제어·로봇·시스템학회 2016 International Journal of Control, Automation, and Vol.14 No.5
In this paper, an Integrated Guidance and Control (IGC) algorithm based on a reference model is proposedfor a side-jet missile. First, a IGC structure is introduced, incorporating the response characteristics of the missilecontrol loop into the guidance loop. To describe the response characteristics, then a reference model is built. Next,with the back stepping scheme and sliding mode control algorithm, the reference model is adopted to derive a novelguidance law, which contains response parameters of missile control system to formulate the IGC design. Finally,simulations and comparisons with the time-scale separation design and an existing IGC design, are conducted toverify the proposed IGC algorithm. It can be shown that the proposed algorithm performs better against highlymaneuvering target in different missile-target initial position and heading scenarios.