Research of Control Strategy for Ducted Rockets
Received date: 2015-08-28
Online published: 2025-05-30
牛文玉 , 刘顶新 . 固体火箭冲压发动机控制方案研究[J]. 弹箭与制导学报, 2016 , 36(4) : 63 -66,69 . DOI: 10.15892/j.cnki.djzdxb.2016.04.017
By setting different margin limiting functions to prevent ramjet from operating in unacceptable regions, control system must permit thrust modulation in a range as wide as possible without exceeding these operating constraints so that overall vehicle performance can be optimized. In this article, control difficulties of ducted rocket were analyzed. Four control strategies for ducted rockets were presented and compared. The study can be used to provide reference for selecting control strategy of ducted rockets.
Key words： ducted rocket; margin limiting function; control strategy
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