TY - JOUR
T1 - Dynamic loading and mission abort decisions considering abort restrictions
AU - Wang, Yuning
AU - Zhao, Xian
AU - Han, He
AU - Qiu, Qingan
N1 - Publisher Copyright:
© IMechE 2025.
PY - 2025
Y1 - 2025
N2 - Considerable attention has been given to load adjustment and mission abort strategies, aimed at striking a balance between advancing mission success and mitigating system failure risk. Existing studies predominantly center on optimizing loading and abort policies without factoring in potential constraints governing abort decisions. In practice, however, there are instances where aborting the mission is not viable during specific stages. For example, submarines may be prohibited from aborting missions and surfacing for rescue operations due to confidentiality reasons. This paper investigates the joint optimization of condition-based mission abort and dynamic load adjustment strategies, while considering limitations on aborting missions. Specifically, the load is dynamically modified based on mission progress and system condition, and missions are terminated during permissible stages to ensure system safety. An example of an integrated minesweeper vehicle is used to illustrate the proposed model and obtained results.
AB - Considerable attention has been given to load adjustment and mission abort strategies, aimed at striking a balance between advancing mission success and mitigating system failure risk. Existing studies predominantly center on optimizing loading and abort policies without factoring in potential constraints governing abort decisions. In practice, however, there are instances where aborting the mission is not viable during specific stages. For example, submarines may be prohibited from aborting missions and surfacing for rescue operations due to confidentiality reasons. This paper investigates the joint optimization of condition-based mission abort and dynamic load adjustment strategies, while considering limitations on aborting missions. Specifically, the load is dynamically modified based on mission progress and system condition, and missions are terminated during permissible stages to ensure system safety. An example of an integrated minesweeper vehicle is used to illustrate the proposed model and obtained results.
KW - Load level adjustment
KW - mission abort policy
KW - mission success probability
KW - shock model
KW - system failure probability
UR - http://www.scopus.com/inward/record.url?scp=105002065705&partnerID=8YFLogxK
U2 - 10.1177/1748006X251327708
DO - 10.1177/1748006X251327708
M3 - Article
AN - SCOPUS:105002065705
SN - 1748-006X
JO - Proceedings of the Institution of Mechanical Engineers, Part O: Journal of Risk and Reliability
JF - Proceedings of the Institution of Mechanical Engineers, Part O: Journal of Risk and Reliability
ER -