Paper
6 February 2022 Mission safety modeling based on SST
Yujin Chen, Jihui Xu, Xiaolin Wang, Xiefeng Wang
Author Affiliations +
Proceedings Volume 12081, Sixth International Conference on Electromechanical Control Technology and Transportation (ICECTT 2021); 1208111 (2022) https://doi.org/10.1117/12.2624718
Event: Sixth International Conference on Electromechanical Control Technology and Transportation (ICECTT 2021), 2021, Chongqing, China
Abstract
The root cause of mission safety problem is the loose combination of safety and mission, and the inadequate traction and restraint of safety by missions. Therefore, an aviation equipment mission safety model is established to study the safety events during mission execution. The definition of mission safety (MS) and the mathematical foundation of the instability domain is given based on the Safety Structure Theory (SST) and three-way decision-making theory(3WD). Factors are used to express the SHEL system and mission system, and then the atomic action factor space (AAFS) is developed to “bear” the state space of the target mission profile, and the atomic SHEL space (ASFS) is developed to “bear” the state space that describes the constraints of the mission system on the SHEL system. The mapping from ASFS×AAFS to ASFS is established, which could transform the evolution of MS into the spatial dynamic trajectory in ASFS. This model can be used in the construction of mission safety analysis platform, the evaluation and prediction.
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Yujin Chen, Jihui Xu, Xiaolin Wang, and Xiefeng Wang "Mission safety modeling based on SST", Proc. SPIE 12081, Sixth International Conference on Electromechanical Control Technology and Transportation (ICECTT 2021), 1208111 (6 February 2022); https://doi.org/10.1117/12.2624718
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KEYWORDS
Safety

Binary data

Safety equipment

Space operations

Mathematical modeling

Logic

Instrument modeling

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