Digital twin system of spaceflight launching site

• Main Authors: WANG SANQIANG, ZUO YUQIN
• Format: Patent
• Language: Chinese; English
• Published: 22.12.2023
• Subjects: AIRCRAFT; AVIATION; CALCULATING; COMPUTING; COSMONAUTICS; COUNTING; DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FORADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORYOR FORECASTING PURPOSES; ELECTRIC DIGITAL DATA PROCESSING; PERFORMING OPERATIONS; PHYSICS; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE,COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTINGPURPOSES, NOT OTHERWISE PROVIDED FOR; TRANSPORTING; VEHICLES OR EQUIPMENT THEREFOR

The invention discloses a digital twin system of a spaceflight launch site, which comprises a data acquisition module, a launch auxiliary module, a launch module and a drop point simulation module, and is characterized in that the data acquisition module comprises a scene modeling system, an air temperature and humidity simulation module, an air temperature and humidity change simulation system, a wind speed simulation module and a wind speed change simulation module; the launching auxiliary module comprises a ground command module, a ground operation module, a spaceflight launching module and a sound effect simulation module, and the launching module comprises a rocket loading module, a fuel filling module, an ignition module and a track trimming module. The system has the beneficial effects that the data acquisition module, the launching auxiliary module, the launching module and the drop point simulation module simulate the occurrence scene of the spacecraft, launch of the spacecraft is simulated in a math