Paper information

Paper code

IAC-22,C1,1,4,x71948

Date

2022-09-18

Time

16:00

Order

4

Room

S05

Title

Fuzzy-Logic-Based Integrated Orbit-Attitude-Vibration Prescribed-Time Control for Large-Scale Flexible Spacecraft

abstract

View PDF

Session

1. Attitude Dynamics (1)

symposium

C1. IAF ASTRODYNAMICS SYMPOSIUM

congress

IAC-22

Type of presentation

oral

Main author

Mr. Bailiang Lyu, Northwestern Polytechnical University, China

Co-authors

Prof. Xiaokui Yue, Northwestern Polytechnical University, China;

Dr. Chuang Liu, Northwestern Polytechnical University, China;