Aircraft attack angle correction curve acquisition method

The invention relates to an aircraft attack angle correction curve acquisition method. The method comprises the steps that step one, the measuring range and the type of an attack angle sensor are selected; step two, the installing area of the attack angle sensor is determined; step three, the instal...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	DENG AIGUO, MA TAO, YANG HAIYAN, LIU ZHONGPING, BAI JUNFENG, CHEN CHANGZHONG, LI YING, LIANG FENGXIA, SHENG JINGRU, ZHANG WEIXIA
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT MEASURING MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK PERFORMING OPERATIONS PHYSICS TESTING TRANSPORTING
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!