TY - JOUR
T1 - Flexible calorimetric flow sensor with unprecedented sensitivity and directional resolution for multiple flight parameter detection
AU - Gong, Zheng
AU - Di, Weicheng
AU - Jiang, Yonggang
AU - Dong, Zihao
AU - Yang, Zhen
AU - Ye, Hong
AU - Zhang, Hengrui
AU - Liu, Haoji
AU - Wei, Zixing
AU - Tu, Zhan
AU - Li, Daochun
AU - Xiang, Jinwu
AU - Ding, Xilun
AU - Zhang, Deyuan
AU - Chen, Huawei
N1 - Publisher Copyright:
© The Author(s) 2024.
PY - 2024/12
Y1 - 2024/12
N2 - The accurate perception of multiple flight parameters, such as the angle of attack, angle of sideslip, and airflow velocity, is essential for the flight control of micro air vehicles, which conventionally rely on arrays of pressure or airflow velocity sensors. Here, we present the estimation of multiple flight parameters using a single flexible calorimetric flow sensor featuring a sophisticated structural design with a suspended array of highly sensitive vanadium oxide thermistors. The proposed sensor achieves an unprecedented velocity resolution of 0.11 mm·s−1 and angular resolution of 0.1°. By attaching the sensor to a wing model, the angles of attack and slip were estimated simultaneously. The triaxial flight velocities and wing vibrations can also be estimated by sensing the relative airflow velocity due to its high sensitivity and fast response. Overall, the proposed sensor has many promising applications in weak airflow sensing and flight control of micro air vehicles.
AB - The accurate perception of multiple flight parameters, such as the angle of attack, angle of sideslip, and airflow velocity, is essential for the flight control of micro air vehicles, which conventionally rely on arrays of pressure or airflow velocity sensors. Here, we present the estimation of multiple flight parameters using a single flexible calorimetric flow sensor featuring a sophisticated structural design with a suspended array of highly sensitive vanadium oxide thermistors. The proposed sensor achieves an unprecedented velocity resolution of 0.11 mm·s−1 and angular resolution of 0.1°. By attaching the sensor to a wing model, the angles of attack and slip were estimated simultaneously. The triaxial flight velocities and wing vibrations can also be estimated by sensing the relative airflow velocity due to its high sensitivity and fast response. Overall, the proposed sensor has many promising applications in weak airflow sensing and flight control of micro air vehicles.
UR - https://www.scopus.com/pages/publications/85189956201
U2 - 10.1038/s41467-024-47284-7
DO - 10.1038/s41467-024-47284-7
M3 - 文章
C2 - 38600119
AN - SCOPUS:85189956201
SN - 2041-1723
VL - 15
JO - Nature Communications
JF - Nature Communications
IS - 1
M1 - 3091
ER -