Missile rolling attitude control method added with integrator dynamic amplitude limiting

The invention discloses a missile rolling attitude control method with integrator dynamic amplitude limiting, and belongs to the technical field of flight control. The method comprises the steps that a guidance instruction resolving unit calculates a rolling instruction of a missile and sends the ro...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SHEN FENG, YU SHUAIXIAN, JIN YIHUAN, ZHENG ZIYUAN, TIAN YE
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PHYSICS REGULATING
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