Integrated guidance and control based on backstepping and high-gain observers

This paper considers the interception of maneuvering targets in the plane. A novel robust nonlinear integrated guidance and control (IGC) law is proposed based on backstepping and high-gain observers to nullify line-of-sight(LOS) rate with taking both missile model uncertainties and target maneuvers...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Yu Bin-Feng, Yan Han, Ji Hai-Bo
Format:	Tagungsbericht
Sprache:	chi ; eng
Schlagworte:	Aerodynamics Automation Backstepping Electronic mail High-Gain Observer Integrated Guidance and Control Missiles Observers Uncertainty
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