Turnover and tail end control semi-physical simulation test method

The invention relates to a turnover and end control semi-physical simulation test method, which comprises the following steps of: designing corresponding control logic according to control requirements of different stages of an aircraft; in the initial launching stage, inertial smoothing is carried...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	ZHENG HONGHAI, YIN CHUNHUI, WANG WU, LI WEI, GONG SANLI, ZOU XIAOXIA, LI WENYANG, HUANG GUIMING, LIU JING, CHEN JIEJING, RAO TINGTING
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
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!