Paper information

Paper code

IAC-26,C1,1,4,x109759

Date

2026-10-05

Time

17:15

Order

4

Room

Hall 8

Title

Three-Axis Attitude Control and Vibration Suppression \\ for Spacecraft with Flexible Structures: \\ An Approach Using Decoupled Optimal Servo Control (DECOPS)

abstract

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Session

1. Attitude Dynamics (1)

symposium

C1. IAF ASTRODYNAMICS SYMPOSIUM

congress

IAC-26

Type of presentation

oral

Main author

Mr. Yuto Yamamoto, Osaka Metropolitan University, Japan

Co-authors

Prof. Sayaka Kanata, Osaka Metropolitan University, Japan;

Prof. Takashi Shimomura, Osaka Metropolitan University, Japan;