Capturability of 3D PPN Against Lower-Speed Maneuvering Target for Homing Phase

被引：37

作者：

Li, Ke-Bo ^{[1
]}

Shin, Hyo-Sang ^{[2
]}

Tsourdos, Antonios ^{[2
]}

Tahk, Min-Jea ^{[3
]}

机构：

[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Dept Appl Mech, Changsha 410073, Peoples R China

[2] Cranfield Univ, SATM, Inst Aerosp Sci, Cranfield MK43 0AL, Beds, England

[3] Korea Adv Inst Sci & Technol, Dept Aerosp Engn, Daejeon 305701, South Korea

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2020年 / 56卷 / 01期

基金：

中国国家自然科学基金;

关键词：

Three-dimensional displays; Missiles; Two dimensional displays; Acceleration; Kinematics; Navigation; Complexity theory; Capturability; nonlinear output regulation method; lower maneuvering target; three-dimensional pure proportional navigation (3-D PPN); GUIDANCE LAW; PROPORTIONAL NAVIGATION; PERFORMANCE ANALYSIS; MISSILE;

D O I：

10.1109/TAES.2019.2938601

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The capturability of the two-dimensional (2-D) pure proportional navigation (PPN) guidance law against lower speed arbitrarily maneuvering target for homing phase had been thoroughly analyzed by using the nonlinear output regulation (NOR) method before. However, due to the complexity of the 3-D relative kinematics, the NOR method has not been applied to the capturability analysis of the 3-D PPN, which leads to the capturability discrepancy of the 2-D PPN and its 3-D extension. Thanks to the 3-D relative kinematic equation between the missile and target established in the rotating line-of-sight coordinate system, the capturability of the 3-D PPN against the lower speed arbitrarily maneuvering target for the homing phase is restudied by extending the NOR method of the 2-D PPN to the 3-D space. The necessary and sufficient condition for the missile guided by the 3-D PPN to intercept this type of target is obtained. It is proven that the capturability of the 3-D PPN is identical with that of the 2-D PPN.

引用

页码：711 / 722

页数：12

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