兵工自动化
兵工自動化
병공자동화
ORDNANCE INDUSTRY AUTOMATION
2014年
1期
89-90,96
,共3页
PID%专家PID%滚转导弹%过载控制
PID%專傢PID%滾轉導彈%過載控製
PID%전가PID%곤전도탄%과재공제
PID%expert PID%roll missile%overload control
针对滚转导弹俯仰和偏航通道较强的气动不确定性和运动耦合，设计了一种专家 PID控制系统。建立了滚转导弹的动力学模型，并采用十字舵来控制俯仰和偏航通道，利用专家 PID控制方法设计该导弹的控制系统，并在Matlab中对控制系统进行仿真。仿真结果表明：该控制器能满足良好的性能要求，具有较强的鲁棒性和自适应性，能有效应对俯仰和偏航通道产生较强气动和运动耦合。
針對滾轉導彈俯仰和偏航通道較彊的氣動不確定性和運動耦閤，設計瞭一種專傢 PID控製繫統。建立瞭滾轉導彈的動力學模型，併採用十字舵來控製俯仰和偏航通道，利用專傢 PID控製方法設計該導彈的控製繫統，併在Matlab中對控製繫統進行倣真。倣真結果錶明：該控製器能滿足良好的性能要求，具有較彊的魯棒性和自適應性，能有效應對俯仰和偏航通道產生較彊氣動和運動耦閤。
침대곤전도탄부앙화편항통도교강적기동불학정성화운동우합，설계료일충전가 PID공제계통。건립료곤전도탄적동역학모형，병채용십자타래공제부앙화편항통도，이용전가 PID공제방법설계해도탄적공제계통，병재Matlab중대공제계통진행방진。방진결과표명：해공제기능만족량호적성능요구，구유교강적로봉성화자괄응성，능유효응대부앙화편항통도산생교강기동화운동우합。
Due to the rolling missile pitch and yaw channels generate strong aerodynamic uncertainty and kinematic coupling, the control system of expert PID is designed. At first, build the dynamic model of rolling missile, at second use cruciform of rudders to control the pitch and yaw channels, then design the control system of rolling missile based on expert PID. At last simulate the control system in a matlab environment. The simulation results show that the controllers can meet performance requirements, it also has better robustness and adaptability which effectively respond to the pitch and yaw channels strong aerodynamic and kinematic coupling.
