Design of EKV Sliding Mode Guidance Law Based on Terminal Angle Limit

A guidance method based on terminal angle limit was researched. By deduction, the relationship between target velocity direction and LOS angle velocity was found in LOS coordinate system, and intercept model based on terminal angle limit was built. Furthermore, on the basis of model nonlinearity, th...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	Danjian yu Zhidao Xuebao / Journal of Projectiles, Rockets, Missiles and Guidance Rockets, Missiles and Guidance, 2015-10, Vol.35 (5), p.22-29
Hauptverfasser:	Nie, Chuang, Shu, Jiansheng, Meng, Shaofei
Format:	Artikel
Sprache:	chi
Schlagworte:	Computer simulation Design engineering Guidance (motion) Missiles Nonlinearity Rockets Sliding mode Terminals
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!