Human-chair system ejection integrated simulation method

The invention discloses a man-chair system ejection integrated simulation method. The method comprises the following steps: inputting initial motion parameters of an aircraft; the body movement module calculates initial movement parameters of the human-chair system; the ejection module calculates mo...

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Bibliographische Detailangaben
Hauptverfasser:	JI XIABIN, TAN SHUAI, FU WENXING, KIM LEEYOUNG, ZHANG RUIXIN, XU HANG
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIRCRAFT AVIATION CALCULATING COMPUTING CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING COSMONAUTICS COUNTING DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ELECTRIC DIGITAL DATA PROCESSING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR MEASURING MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PERFORMING OPERATIONS PHYSICS REGULATING TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR TRANSPORTING
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Beschreibung
Zusammenfassung:	The invention discloses a man-chair system ejection integrated simulation method. The method comprises the following steps: inputting initial motion parameters of an aircraft; the body movement module calculates initial movement parameters of the human-chair system; the ejection module calculates motion parameters of the human-chair system and then outputs the motion parameters to the navigation module; the navigation module converts motion parameters of the human-chair system into a navigation coordinate system and feeds back the motion parameters to the environment module; the environment module provides gravitational acceleration for the ejection cabin-out module; after ejection out of the cabin, the free flight module solves motion parameters of the human-chair system and feeds back the motion parameters to the navigation module; the navigation module converts motion parameters of the human-chair system to a navigation coordinate system and transmits the motion parameters to the free flight module through