Attitude Stabilization of a Flexible Satellite with Sloshing Phenomenon-Reference-Cited by-同舟云学术

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Attitude Stabilization of a Flexible Satellite with Sloshing Phenomenon

Published:2023-10-21 Issue: Volume: Page:
ISSN:
Container-title:2023 International Conference on Networking and Advanced Systems (ICNAS)
language:
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Author:

Benmansour Jalal Eddine¹,Roubache Rima²,Khouane Boulanouar³

Affiliation:

1. Research Satellite Development Center,Department of Spcace Mechanics,Oran,Algeria

2. Research Satellite Development Center,Department of Space Mechanics,Oran,Algeria

3. Satellite Development Center,Department of Space Mission and Systems,Oran,Algeria

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10330163/10330438/10330508.pdf?arnumber=10330508

Reference20 articles.

1. Active Vibration Suppression in Flexible Spacecraft Attitude Tracking

2. Output stabilization of flexible spacecraft with active vibration suppression

3. Positive position feedback control for large space structures

4. Vibration suppression of flexible spacecraft during attitude control

5. Spacecraft Vibration Reduction Using Pulse-Width Pulse-Frequency Modulated Input Shaper

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