Affiliation of Author(s):航天学院
Journal:Adv. Space Res.
Abstract:The capability of autonomous fault detection and reconstruction is essential for future manned Mars exploration missions. Considering actuator failures and atmosphere uncertainties, we present a new active fault-tolerant control algorithm for Mars entry by use of neural network and structure adaptive model inversion. First, the online BP neural network is adopted to conduct the fault detection and isolation. Second, based on the structure adaptive model inversion, an adaptive neural network PID controller is developed for Mars entry fault-tolerant control. The normal PID controller will be automatically switched into neural network PID controller when an actuator fault is detected. Therefore, the error between the reference model and the output of the attitude control system would be adjusted to ensure the dynamic property of the entry vehicle. Finally, the effectiveness of the algorithm developed in this paper is confirmed by computer simulation. © 2018 COSPAR
ISSN No.:0273-1177
Translation or Not:no
Date of Publication:2019-01-01
Co-author:Huang, Yixin,Sun, Jun
Correspondence Author:李爽
Professor
Alma Mater:哈尔滨工业大学
Education Level:哈尔滨工业大学
Degree:Doctoral Degree in Engineering
School/Department:College of Astronautics
Discipline:Flight Vehicle Design. Guidance, Navigation, and Control
Business Address:江宁校区D11号楼A503
Contact Information:025-84896039
Open time:..
The Last Update Time:..