TY - GEN
T1 - Fault-Tolerant Integrated Guidance and Control Design for Hypersonic Vehicle Based on ADRC
AU - Yan, Guocheng
AU - Wang, Honglun
AU - Wu, Tiancai
AU - Wu, Xingyu
N1 - Publisher Copyright:
© Beijing HIWING Scientific and Technological Information Institute 2024.
PY - 2024
Y1 - 2024
N2 - To ensure the stability and safety of hypersonic vehicle reentry flights, we have designed a fault-tolerant integrated guidance and control (FTIGC) system using active disturbance rejection control (ADRC) theory. This system takes into account the presence of multiple uncertain factors and potential actuator malfunctions, which could compromise the vehicle’s trajectory. First, to tackle the issue of error caused by the association between individual guidance and control loop designs, a 6 DOF model of hypersonic vehicles and fault model of actuator are established. Then, predictor-corrector guidance law based on quasi-equilibrium glide condition (QEGC) is employed in guidance loop. In fault-tolerant control system, active disturbance rejection controllers are designed in attitude loop and angular loop respectively. Finally, under the condition of without and with actuator faults, the simulations are conducted. The effectiveness of the FTIGC system based on ADRC theory is verified through the simulation result.
AB - To ensure the stability and safety of hypersonic vehicle reentry flights, we have designed a fault-tolerant integrated guidance and control (FTIGC) system using active disturbance rejection control (ADRC) theory. This system takes into account the presence of multiple uncertain factors and potential actuator malfunctions, which could compromise the vehicle’s trajectory. First, to tackle the issue of error caused by the association between individual guidance and control loop designs, a 6 DOF model of hypersonic vehicles and fault model of actuator are established. Then, predictor-corrector guidance law based on quasi-equilibrium glide condition (QEGC) is employed in guidance loop. In fault-tolerant control system, active disturbance rejection controllers are designed in attitude loop and angular loop respectively. Finally, under the condition of without and with actuator faults, the simulations are conducted. The effectiveness of the FTIGC system based on ADRC theory is verified through the simulation result.
KW - Fault-Tolerant Control
KW - Hypersonic Vehicle
KW - Integrated Guidance and Control
UR - https://www.scopus.com/pages/publications/85192521273
U2 - 10.1007/978-981-97-1107-9_48
DO - 10.1007/978-981-97-1107-9_48
M3 - 会议稿件
AN - SCOPUS:85192521273
SN - 9789819711062
T3 - Lecture Notes in Electrical Engineering
SP - 517
EP - 526
BT - Proceedings of 3rd 2023 International Conference on Autonomous Unmanned Systems (3rd ICAUS 2023) - Volume I
A2 - Qu, Yi
A2 - Gu, Mancang
A2 - Niu, Yifeng
A2 - Fu, Wenxing
PB - Springer Science and Business Media Deutschland GmbH
T2 - 3rd International Conference on Autonomous Unmanned Systems, ICAUS 2023
Y2 - 9 September 2023 through 11 September 2023
ER -