Aircraft mathematical simulation software framework automatic construction method

• Main Authors: TIE MING, LI MINGJUN, ZOU XU, WU XUSHENG, CHEN SUFANG, MA YILEI, WANG JIANLIN, YU YING, ZHU XIUJUAN, ZHANG JUN, LIANG WEIDONG, LIU JING
• Format: Patent
• Language: Chinese; English
• Published: 16.12.2022
• Subjects: CALCULATING; COMPUTING; COUNTING; ELECTRIC DIGITAL DATA PROCESSING; PHYSICS

The invention provides an aircraft mathematical simulation software framework automatic construction method, and belongs to the technical field of system simulation, and the method comprises the following steps: S1, packaging each subject model, and storing information in a model library; s2, reading a graphical simulation process description file; s3, DTD constraint verification is carried out on the file; if the file is invalid, executing S13; if so, executing S4; s4, analyzing the file; s5, connecting the model library, and if the connection fails, executing S13; if the connection is successful, executing S6; s6, information obtained through analysis in the step S3 is obtained from the model library; s7, checking whether input and output are matched or not; s8, if the connection rule is not met, executing S13; if yes, executing S9; s9, determining an execution sequence of each model; s10, generating a basic simulation program framework; s11, adding a calling code for a model initialization function; and S1