四川兵工学报
四川兵工學報
사천병공학보
SICHUAN ORDNANCE JOURNAL
2011年
8期
52-55,58
,共5页
于德海%范作娥%史贤俊%顾文锦
于德海%範作娥%史賢俊%顧文錦
우덕해%범작아%사현준%고문금
落角%模糊%导引律%反舰导弹
落角%模糊%導引律%反艦導彈
락각%모호%도인률%반함도탄
impact angle%fuzzy%guidance law%anti-ship missile
为了完成反舰导弹按预定方向打击目标的战术要求,基于三维弹目相对运动模型,将落角要求约束在滑模面上,然后通过模糊系统对非线性模型进行逼近,设计了一种带有落角约束的三维自适应模糊滑模导引,并根据Lyapunov稳定性定理,从理论上证明了制导系统的稳定性。仿真结果表明了本文方法的正确性和有效性。
為瞭完成反艦導彈按預定方嚮打擊目標的戰術要求,基于三維彈目相對運動模型,將落角要求約束在滑模麵上,然後通過模糊繫統對非線性模型進行逼近,設計瞭一種帶有落角約束的三維自適應模糊滑模導引,併根據Lyapunov穩定性定理,從理論上證明瞭製導繫統的穩定性。倣真結果錶明瞭本文方法的正確性和有效性。
위료완성반함도탄안예정방향타격목표적전술요구,기우삼유탄목상대운동모형,장락각요구약속재활모면상,연후통과모호계통대비선성모형진행핍근,설계료일충대유락각약속적삼유자괄응모호활모도인,병근거Lyapunov은정성정리,종이론상증명료제도계통적은정성。방진결과표명료본문방법적정학성화유효성。
In order to achieve the tactical mission of accurately attacking the target,based on relative motion model of missile and target,a 3-D adaptive fuzzy sliding mode guidance law with impact angle constraint is proposed by constraining the impact angle on the sliding mode,and the anti-ship missile model is approximated by fuzzy system in case that the precise nonlinear model is not obtained.The stability of the guidance system is theoretically proved by Lyapunov stability theory.The numerical simulation result shows the validity and effectiveness of the proposed method.