CAJ | 학술논문

为满足反作用控制系统(reaction control system，RCS)姿态控制需求，对高超声速飞行器再入段的姿态控制进行研究。以X-34的RCS系统为对象，建立了RCS的数字模型，设计了RCS姿态控制率与PWPE脉冲调制器，利用非线性描述函数法分析姿态控制系统的稳定性，并通过 Matlab 仿真验证了所设计的 RCS 姿态控制系统性能。仿真结果表明：该PWPF脉冲调制可以满足RCS姿态控制的需要，同时与传统的PWM脉冲调制相比，可以较大地降低RCS消耗的流量与开启次数，可为高超声速飞行器再入段RCS姿态控制系统设计提供参考。
위만족반작용공제계통(reaction control system，RCS)자태공제수구，대고초성속비행기재입단적자태공제진행연구。이X-34적RCS계통위대상，건립료RCS적수자모형，설계료RCS자태공제솔여PWPE맥충조제기，이용비선성묘술함수법분석자태공제계통적은정성，병통과 Matlab 방진험증료소설계적 RCS 자태공제계통성능。방진결과표명：해PWPF맥충조제가이만족RCS자태공제적수요，동시여전통적PWM맥충조제상비，가이교대지강저RCS소모적류량여개계차수，가위고초성속비행기재입단RCS자태공제계통설계제공삼고。
In order to meet the attitude control requirement of reaction control system (RCS), research on attitude control of reaction control system for hypersonic vehicle. Taking the RCS of X-34 as object, establish RCS mathematical model, design RCS attitude control rate and PWPE pulse modulator. Analysis the stabilization of RCS attitude control system using nonlinearity describing function method, and validate RCS attitude control performance through Matlab. The simulation results show that the PWPF modulator not only can meet RCS attitude control’s requirement, but also can reduce RCS flow consumption and jet times compared with traditional PWM pulse modulation. The method can offer reference for attitude control of reaction control system for hypersonic vehicle.