Paper information

Paper code

IAC-21,C1,1,10,x64510

Date

2021-10-25

Time

17:15

Order

1010

Room

Sheikh Maktoum C

Title

Dual-quaternion based finite-time adaptive control for spacecraft autonomous proximity maneuver with pyramid-type constraints

abstract

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Session

1. Guidance, Navigation and Control (1)

symposium

C1. IAF ASTRODYNAMICS SYMPOSIUM

congress

IAC-21

Type of presentation

oral

Main author

Mrs. Liangyue Wang, Harbin Institute of Technology, China

Co-authors

Dr. Yanning Guo, Harbin Institute of Technology, China;

Prof. Guangfu Ma, China;

Mr. yueyong LYU, Harbin Institute of Technology, China;

Dr. Haibo Zhang, 1.Beijing Institute of Control Engineering, 2.National Key Laboratory of Science and Technology on Space Intelligent Control, China, China;