海军航空工程学院学报Issue(4)：368-372,5.DOI:10.7682/j.issn.1673-1522.2013.04.007
带落角和末端攻角约束的最优末制导律
Optimal Guidance Law with Constraint on Terminal Impact Angle and Angle of Attack
摘要
Abstract
In order to meet the requirements of the missile high-precision guilded. The considering the condi-tions under the constraints with the impact angle and the angle of attack, the new guidance law was deduced by the quadratic optimal control. The verified results showed that the guidance law with the impact angle and the angle of attack constraint was satisfied not only the requirements of high-precision guidance, but also the end of attack could be a good control.关键词
落角约束/末端攻角约束/制导律/最优控制Key words
terminal impact angular constriaint/constraint of terminal angle of attack/guidance law/optimal con-trol分类
武器工业引用本文复制引用
张友安,孙阳平,方悦,黄诘..带落角和末端攻角约束的最优末制导律[J].海军航空工程学院学报,2013,(4):368-372,5.基金项目
国家自然科学基金资助项目（61273058）；海军航空工程学院研究生创新基金资助项目 （）
