系统工程与电子技术
繫統工程與電子技術
계통공정여전자기술
SYSTEMS ENGINEERING AND ELECTRONICS
2015年
7期
1604-1610
,共7页
制导控制一体化%自抗扰控制%扩张状态观测器%反步终端滑模
製導控製一體化%自抗擾控製%擴張狀態觀測器%反步終耑滑模
제도공제일체화%자항우공제%확장상태관측기%반보종단활모
integrated guidance and control%active disturbance rejection control%extended state observer%backstepping terminal sliding mode
针对导弹末制导段的制导控制问题，基于自抗扰控制和反演终端滑模控制，提出了一种导弹制导控制一体化设计算法。利用块严格反馈系统描述一体化模型，将存在的模型误差、目标机动等看做未知干扰。采用扩张状态观测器对系统不确定性和干扰进行估计和补偿。设计反步终端滑模控制方法实现导弹的姿态控制。仿真证明了设计的一体化算法可以获得较小的脱靶量，系统对存在的内外干扰和不确定性具有较强的鲁棒性。
針對導彈末製導段的製導控製問題，基于自抗擾控製和反縯終耑滑模控製，提齣瞭一種導彈製導控製一體化設計算法。利用塊嚴格反饋繫統描述一體化模型，將存在的模型誤差、目標機動等看做未知榦擾。採用擴張狀態觀測器對繫統不確定性和榦擾進行估計和補償。設計反步終耑滑模控製方法實現導彈的姿態控製。倣真證明瞭設計的一體化算法可以穫得較小的脫靶量，繫統對存在的內外榦擾和不確定性具有較彊的魯棒性。
침대도탄말제도단적제도공제문제，기우자항우공제화반연종단활모공제，제출료일충도탄제도공제일체화설계산법。이용괴엄격반궤계통묘술일체화모형，장존재적모형오차、목표궤동등간주미지간우。채용확장상태관측기대계통불학정성화간우진행고계화보상。설계반보종단활모공제방법실현도탄적자태공제。방진증명료설계적일체화산법가이획득교소적탈파량，계통대존재적내외간우화불학정성구유교강적로봉성。
Based on active disturbance rejection control and the backstepping-sliding mode design method, an integrated guidance and control design is proposed for missiles during the terminal course.The integrated model is formulated as a block-strict-feedback nonlinear system,in which modeling errors and target maneuvers are viewed as unknown uncertainties.An extended state observer is developed to estimate and compensate the impact from uncertainties and disturbances.A backstepping-sliding mode controller is proposed to realize the at-titude control.Simulation results show that,with the application of the proposed method,small miss distances are achieved,and the system is robust against system uncertainties and disturbances.
