Rocket testing method and device, electronic equipment and computer readable storage medium

• Main Authors: ZHANG SHIQIANG, HUI XINGCHEN, CHEN XI, XUN FEI, TONG MINGXI, CONG ENBO, XIAO XUE, YE ZHIPENG, LIU SIQI, GUAN HONGREN, BIAN XU, WANG ZHENGHAN, ZHOU XIANTAO, ZHANG DONGLIANG, HE LEI, MA XIAOJING, YAO YAO, ZHANG GUOFENG, LIU WEI, LI HAOWEI, LIU JIAJIA, QI HUAN, WANG JINING, WU ZHOUHANG, ZHANG JING, XING ZHI, JIN XIN, MA SHANG, ZHANG WEN, ZHANG ZHONGZHOU, JIA YINGHE
• Format: Patent
• Language: Chinese; English
• Published: 16.08.2024
• Subjects: AMMUNITION; BLASTING; EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION; HEATING; LIGHTING; MECHANICAL ENGINEERING; WEAPONS

The invention discloses a rocket testing method and device, electronic equipment and a computer readable storage medium, and relates to the technical field of spaceflight and the technical field of rocket launching. The method comprises the following steps: acquiring target test data of a target parameter of a target rocket in a preset time period; detecting whether the target test data meets a first test rule and a second test rule; under the condition that the target test data meet the first test rule and the second test rule at the same time, determining that the target test data is normal data and the target parameters of the target rocket pass the test; and under the condition that the target test data does not meet the first test rule and/or the second test rule, determining that the target test data is abnormal data and the target parameter of the target rocket does not pass the test. The technical problem of low rocket test efficiency caused by judging whether the rocket parameters pass the test based