TY - JOUR
T1 - Vibration suppression of flexible hose for autonomous aerial refueling based on adaptive boundary compound controller
AU - Hang, Bin
AU - Xu, Bin
N1 - Publisher Copyright:
© 2024 Elsevier Masson SAS
PY - 2024/11
Y1 - 2024/11
N2 - The suppression of vibrations in flexible hoses during autonomous aerial refueling (AAR) is crucial for enhancing mission success rates and safety, advancing AAR technology. In this paper, an adaptive boundary compound control (ABCC) strategy is proposed to address the vibration suppression problem of the flexible hose of a tanker subject to the bow wave effect (BWE) of the receiver, state output constraint, and partial actuator failure. Unlike previous studies, this research takes into account the impact of the receiver's BWE on these vibrations. The flexible hose is modeled as a three-dimensional Euler-Bernoulli beam (TDEBB), utilizing partial differential equations (PDEs) to provide a more accurate description of its dynamic characteristics. Furthermore, the proposed ABCC strategy accurately detects all disturbances, ensures that the system state output remains within specified limits, and maintains stability even in the face of actuator failures. Last but not least, numerical comparisons and simulations demonstrate that the ABCC method significantly suppresses hose vibrations and maintains end displacement within a narrow range.
AB - The suppression of vibrations in flexible hoses during autonomous aerial refueling (AAR) is crucial for enhancing mission success rates and safety, advancing AAR technology. In this paper, an adaptive boundary compound control (ABCC) strategy is proposed to address the vibration suppression problem of the flexible hose of a tanker subject to the bow wave effect (BWE) of the receiver, state output constraint, and partial actuator failure. Unlike previous studies, this research takes into account the impact of the receiver's BWE on these vibrations. The flexible hose is modeled as a three-dimensional Euler-Bernoulli beam (TDEBB), utilizing partial differential equations (PDEs) to provide a more accurate description of its dynamic characteristics. Furthermore, the proposed ABCC strategy accurately detects all disturbances, ensures that the system state output remains within specified limits, and maintains stability even in the face of actuator failures. Last but not least, numerical comparisons and simulations demonstrate that the ABCC method significantly suppresses hose vibrations and maintains end displacement within a narrow range.
KW - Autonomous aerial refueling
KW - Bow wave effect
KW - Flexible hoses
KW - Partial differential equations
KW - Three-dimensional Euler Bernoulli beam
KW - Vibration suppression
UR - http://www.scopus.com/inward/record.url?scp=85201732927&partnerID=8YFLogxK
U2 - 10.1016/j.ast.2024.109494
DO - 10.1016/j.ast.2024.109494
M3 - 文章
AN - SCOPUS:85201732927
SN - 1270-9638
VL - 154
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 109494
ER -