Journal of System Simulation
Abstract
Abstract: In order to meet the needs of the overall performance simulation and verification of the vehicle with large subsamples and massive states, a high-performance simulation method is proposed, in which a parallel simulation architecture based on high-performance computers is established, the technologies and software such as decoupling of simulation tasks, real-time monitoring of simulation, concurrent conflict control and automatic aggregation of large-scale test results are realized, and a test platform for the large-scale parallel verification of flight performance is developed. Simulation results show that the method has high acceleration ratio and scalability, and can complete the verification efficiently, which not only improves the overall verification and evaluation capability of the vehicle, but also promotes the improvement of the vehicle design.
Recommended Citation
Wang, Jianlin; Chen, Sufang; Ming, Tie; Jing, Liu; and Jun, Zhang
(2021)
"High Performance Simulation Method and Test Platform for Full Envelop of Flight Vehicle,"
Journal of System Simulation: Vol. 33:
Iss.
10, Article 2.
DOI: 10.16182/j.issn1004731x.joss.21-0625
Available at:
https://dc-china-simulation.researchcommons.org/journal/vol33/iss10/2
First Page
2298
Revised Date
2021-08-28
DOI Link
https://doi.org/10.16182/j.issn1004731x.joss.21-0625
Last Page
2306
CLC
TP391.9
Recommended Citation
Wang Jianlin, Chen Sufang, Tie Ming, Liu Jing, Zhang Jun. High Performance Simulation Method and Test Platform for Full Envelop of Flight Vehicle[J]. Journal of System Simulation, 2021, 33(10): 2298-2306.
DOI
10.16182/j.issn1004731x.joss.21-0625
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