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为适应未来导弹高机动、快速反应的需要,提出了应用大功率侧向发动机的导弹联机控制法则及其使用的多点设计方法,通过研究试验和仿真,明确了该控制法则的有效性。
In order to meet the need of high maneuvering and rapid response of future missiles, the article put forward the on-line control law of missile using high-power side-to-side engine and its multi-point design method. Through the experiment and simulation, the effectiveness of the control law is clarified.