海军航空工程学院学报2011，Vol.26Issue(5)：517-520,4.
带落角约束的末端机动Terminal滑模导引律设计
Design of a Maneuver Terminal Sliding Mode Guidance Law with Impact Angle Constraints
摘要
Abstract
In order to improve the penetration effect of the- anti-ship missile, avoid to be intercepted by the ship-to-air missile, and achieve the tactical mission of attacking the target on the appointed direction, based on the 3-D relative motion model of missile and target, a Terminal sliding mode guidance law with impact angle constraints, was presented in the point of view of engineering application. Then a virtual interference was added on the proposed guidance law, and the it had no effect on the stability of the guidance system and the attack precision. The suppositional disturbance can offer the enough acceleration of the anti-ship missile, but not exceed the available acceleration. And the virtual interference could produce certain terminal maneuver to avoid the intercepting of the enemy ship-to-air missile. The numerical simulation result showed the validity and effectiveness of the proposed method.关键词
导引律/Terminal滑模/落角约束/机动Key words
guidance law/Terminal sliding mode/impact angle constraint/maneuver分类
军事科技引用本文复制引用
于德海,范作娥,史贤俊..带落角约束的末端机动Terminal滑模导引律设计[J].海军航空工程学院学报,2011,26(5):517-520,4.基金项目
总装武器装备重点创新基金支持项目 （）
