CAJ | 학술논문

飞行控制系统是智能化精确制导火箭弹的关键部件。结合快速控制原型技术，搭建了制导火箭弹飞行控制半实物仿真系统平台，控制率算法模型可以加载到飞控计算机中，并与舵机伺服系统实物相连，参与硬件在回路仿真实验，使算法在硬件实现之前得到检验。根据半实物仿真试验结果，可以优化控制参数，调整控制策略，完善控制算法，并为控制软件的设计、改进及优化提供了试验环境。最后通过试验验证，该半实物仿真系统运行稳定可靠，实时性强，具有工程应用价值。
비행공제계통시지능화정학제도화전탄적관건부건。결합쾌속공제원형기술，탑건료제도화전탄비행공제반실물방진계통평태，공제솔산법모형가이가재도비공계산궤중，병여타궤사복계통실물상련，삼여경건재회로방진실험，사산법재경건실현지전득도검험。근거반실물방진시험결과，가이우화공제삼수，조정공제책략，완선공제산법，병위공제연건적설계、개진급우화제공료시험배경。최후통과시험험증，해반실물방진계통운행은정가고，실시성강，구유공정응용개치。
Flight control system is a key sector of intelligent precision guided rocket. Using Rapid Control Prototype method,a hardware-in-the-loop simulation platform of flight control system for guided rocket is constructed in this paper. Through this platform,the model of control law algorithm can be downloaded to the flight control computer to achieve hardware-in-the-loop simulation,which makes it possible to design and testify the control strategy before the hardware is available. Based on analyzing the simulation experiments,it also makes contributes to the design,modification and optimization of the control software. Experiments eventually show that the platform could run stably and reliably,and has explicit real-time capability while having engineering applicable value.