TY - CHAP
T1 - Vibration Control of a Flexible Aerial Refueling Hose with Input Saturation
AU - Liu, Zhijie
AU - Liu, Jinkun
N1 - Publisher Copyright:
© 2020, Tsinghua University Press.
PY - 2020
Y1 - 2020
N2 - In Chap. 5, we developed a PDE model for a flexible aerial refueling hose system during coupling. As we know, a hose-drogue aerial refueling system consists of a flexible hose and an active drogue control actuator, which are the most universal refueling equipments of probe-drogue refueling (PDR). The probe and drogue systems are comparatively simpler and more compact than the flying boom, and their arrangement on the tanker enables multiple aircraft to be refueled simultaneously. The significant drawback is that PDR requires a skillful piloting technique of maneuvering a probe into the center of a moving drogue with an acceptable closure rate. However, due to the flexible property of the hose, the deflection of the flexible hose has a significant influence on the dynamics and control performance of the AAR, which brings difficulties to the coupling. In order to solve this problem, we will establish a model for a flexible aerial refueling hose system before coupling, and develop an efficient boundary control scheme to suppress vibrations. Moreover, considering that common active drogue control actuators which consists of a set of aerodynamic control surface [5, 7] or other kinds of controllable drogues [6] cannot provide enough control input, which degrades the performance of the control system or leads to the instability.
AB - In Chap. 5, we developed a PDE model for a flexible aerial refueling hose system during coupling. As we know, a hose-drogue aerial refueling system consists of a flexible hose and an active drogue control actuator, which are the most universal refueling equipments of probe-drogue refueling (PDR). The probe and drogue systems are comparatively simpler and more compact than the flying boom, and their arrangement on the tanker enables multiple aircraft to be refueled simultaneously. The significant drawback is that PDR requires a skillful piloting technique of maneuvering a probe into the center of a moving drogue with an acceptable closure rate. However, due to the flexible property of the hose, the deflection of the flexible hose has a significant influence on the dynamics and control performance of the AAR, which brings difficulties to the coupling. In order to solve this problem, we will establish a model for a flexible aerial refueling hose system before coupling, and develop an efficient boundary control scheme to suppress vibrations. Moreover, considering that common active drogue control actuators which consists of a set of aerodynamic control surface [5, 7] or other kinds of controllable drogues [6] cannot provide enough control input, which degrades the performance of the control system or leads to the instability.
UR - https://www.scopus.com/pages/publications/85083468969
U2 - 10.1007/978-981-15-2596-4_6
DO - 10.1007/978-981-15-2596-4_6
M3 - 章节
AN - SCOPUS:85083468969
T3 - Springer Tracts in Mechanical Engineering
SP - 85
EP - 102
BT - Springer Tracts in Mechanical Engineering
PB - Springer
ER -