上海航天
上海航天
상해항천
AEROSPACE SHANGHAI
2012年
4期
68-72
,共5页
防空导弹%侧向回路%稳定控制结构%过载反馈通道
防空導彈%側嚮迴路%穩定控製結構%過載反饋通道
방공도탄%측향회로%은정공제결구%과재반궤통도
Anti-air missile%Lateral loop%Control structure of stability%Overload feedback channel
基于复合稳定控制结构,对某防空导弹侧向回路过载反馈通道的结构进行了改进。基于理论分析,结合工程应用实际进行了数学仿真验证。结果表明：在保持足够稳定裕度的前提下,改进结构的系统快速性好,鲁棒性更优。
基于複閤穩定控製結構,對某防空導彈側嚮迴路過載反饋通道的結構進行瞭改進。基于理論分析,結閤工程應用實際進行瞭數學倣真驗證。結果錶明：在保持足夠穩定裕度的前提下,改進結構的繫統快速性好,魯棒性更優。
기우복합은정공제결구,대모방공도탄측향회로과재반궤통도적결구진행료개진。기우이론분석,결합공정응용실제진행료수학방진험증。결과표명：재보지족구은정유도적전제하,개진결구적계통쾌속성호,로봉성경우。
The structure of overload feedback channel in lateral loop for some anti-air missile was improved based on the combined stability control structure in this paper. The simulation was made according to the engineering application based on the theory analysis. The results showed that the improved structure had good system rapidity and better robustness under the condition of keeping sufficient stability margin.
