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[an error occurred while processing this directive]Research on Trajectory Modeling and Simulation of Suspended Rocket Based on Solid Rocket Motor
Received date: 2021-10-26
Online published: 2025-05-29
高乔 , 杨军 , 李晓晖 , 张兵峰 . 一种基于固体火箭发动机的悬浮火箭弹道建模与仿真研究[J]. 弹箭与制导学报, 2022 , 42(2) : 100 -104 . DOI: 10.15892/j.cnki.djzdxb.2022.02.018
Aiming at the problem that the ship is attacked by anti-ship missiles on the sea, the suspension rocket is used to guide the missile to the safe area outside the ship. For the working process of suspension rocket, a control scheme is proposed.The first is to use the simulation software to build the six degree of freedom simulation model of the suspension rocket.In order to make the suspension rocket conduct controllable flight in the climbing phase and level flight phase, the dual loop feedback control of damping loop and attitude loop is adopted for the attitude, the dual loop feedback control of “height + speed” is adopted for the altitude, and the dual loop feedback control of “speed + acceleration” is adopted for the speed. The simulation results show that this control scheme is feasible.The suspension rocket can maintain a stable attitude in the suspension stage, and can control the altitude and speed for stable flight. The ballistic characteristics basically meet the requirements.
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