TY - GEN
T1 - Research on Multi-Level Simulation Environment of Aircraft Actuation System Based on Flight Mission Scenarios
AU - Wu, Yan
AU - Li, Yang
AU - Jiang, Linlin
AU - Shang, Yaoxing
N1 - Publisher Copyright:
© 2023 IEEE.
PY - 2023
Y1 - 2023
N2 - In order to meet the operating conditions during full flight profile, aircraft actuation system often increases the design margin of rated operating points, resulting in the waste of aircraft energy. In order to clarify power demand characteristics of aircraft actuation system, a multilevel simulation environment of mission level, aircraft level, system level is modeled in this paper. The simulation environment is based on the real flight mission scenarios, and the closed-loop flight controller is designed on the basis of the aircraft motion equation. Taking an advanced military aircraft as an example, the power demand during the maneuvering process of aircraft is transmitted to the actuation system through the control surfaces. In this paper, power demand characteristics under specific mission scenarios are obtained, which helps to refine the design of aircraft actuation system.
AB - In order to meet the operating conditions during full flight profile, aircraft actuation system often increases the design margin of rated operating points, resulting in the waste of aircraft energy. In order to clarify power demand characteristics of aircraft actuation system, a multilevel simulation environment of mission level, aircraft level, system level is modeled in this paper. The simulation environment is based on the real flight mission scenarios, and the closed-loop flight controller is designed on the basis of the aircraft motion equation. Taking an advanced military aircraft as an example, the power demand during the maneuvering process of aircraft is transmitted to the actuation system through the control surfaces. In this paper, power demand characteristics under specific mission scenarios are obtained, which helps to refine the design of aircraft actuation system.
KW - aircraft actuation system
KW - flight mission scenarios
KW - multilevel simulation environment
UR - https://www.scopus.com/pages/publications/85197559470
U2 - 10.1109/FPM57590.2023.10565598
DO - 10.1109/FPM57590.2023.10565598
M3 - 会议稿件
AN - SCOPUS:85197559470
T3 - 2023 9th International Conference on Fluid Power and Mechatronics, FPM 2023
BT - 2023 9th International Conference on Fluid Power and Mechatronics, FPM 2023
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 9th International Conference on Fluid Power and Mechatronics, FPM 2023
Y2 - 18 August 2023 through 21 August 2023
ER -