Attitude and orbit control engine test process system parameter real-time monitoring system and monitoring method

• Main Authors: GAO MINGHUI, GONG HOUJUAN, LIU QIANG, LIU LINING, XIANG HONGYAN, LI JINGWEN, REN YU, LIU YUFENG, ZHANG SUWEN, ZHANG XIAOYU, BAI YU, WANG WEI, YANG MINLI, XIAO JINGJING, SHU YIHAN, LIU SHEN
• Format: Patent
• Language: Chinese; English
• Published: 01.12.2023
• Subjects: MEASURING; PHYSICS; TESTING; TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR

The invention discloses a real-time monitoring system and a real-time monitoring method for parameters of an attitude and orbit control engine test process system, which are used for solving the technical problems that an existing monitoring method is easy to cause inspection omission and relatively low in inspection efficiency, and related parameters of a propellant or pressurized gas in a storage tank cannot be monitored in real time. The real-time monitoring system provided by the invention comprises a monitoring unit, an acquisition unit, a main control unit and a display unit, the monitoring unit comprises an environmental parameter measuring device installed between propellants in the attitude and orbit control engine test process system, and a sensor unit installed on each storage box between the propellants; the input end of the acquisition unit is respectively connected with the environmental parameter measuring device and the sensor unit, and the output end is connected with the main control unit fo