CAJ | 학술논문

针对导弹姿态控制面临的非线性、参数不确定与外界干扰等问题，研究基于非线性干扰观测器的干扰抑制状态相关的黎卡提方程姿态控制方法。首先，引入总干扰概念，将参数不确定与外界干扰等因素对系统的影响统一看作系统总干扰；然后，通过设计总干扰补偿系数，实现具有非匹配干扰抑制能力的状态相关的黎卡提方程姿态控制系统设计；最后，利用非线性干扰观测器得到系统总干扰的估计值。仿真结果表明，所设计的姿态控制方法能够有效跟踪期望攻角指令，同时对系统参数不确定与外界干扰具有较强的抑制能力。
침대도탄자태공제면림적비선성、삼수불학정여외계간우등문제，연구기우비선성간우관측기적간우억제상태상관적려잡제방정자태공제방법。수선，인입총간우개념，장삼수불학정여외계간우등인소대계통적영향통일간작계통총간우；연후，통과설계총간우보상계수，실현구유비필배간우억제능력적상태상관적려잡제방정자태공제계통설계；최후，이용비선성간우관측기득도계통총간우적고계치。방진결과표명，소설계적자태공제방법능구유효근종기망공각지령，동시대계통삼수불학정여외계간우구유교강적억제능력。
The nonlinear disturbance observer based disturbance rejection SDRE attitude control is investigated for a general nonlinear missile with parameter uncertainties and external disturbances . Firstly , the total effects of the parameter uncertainties and external disturbances are regarded as the lumped disturbances . And then , a disturbance compensation gain is carefully designed , so that the disturbance rejection SDRE attitude control method is able to address the mismatched disturbances . Finally , the nonlinear disturbance observer is introduced to estimate the lumped disturbances . Simulation results have demonstrated the precise tracking performance and the disturbance rejection capability of the proposed method with respect to the parameter uncertainties and external disturbances .