摘要
某型涡轴发动机全权限数控系统采用了状态反馈控制方式.根据内模原理,引入伺服补偿器,使设计的控制系统不仅具有较强的鲁棒性,而且在用于指令跟踪时能消除稳态误差;根据性能指标要求设计了状态反馈控制器,从而提高控制系统的品质.与目前的PID控制方式相比较,半物理模拟试验结果表明该控制方式有显著的性能改进.
A turbo-shaft engine FADEC system is subjected to the state feedback control mode. Based on the internal principle, a servo-compensator was introduced such that the control system could present strong robustness, and also eliminate steady state errors when tracking with commands. According to performance index, a states feedback controller was also designed to improve the performance of the control system. As compared with PID control method,the test results show an outstanding performance of the control system.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
2007年第5期829-832,共4页
Journal of Aerospace Power