Spacecraft Attitude Control using NSTSM and RW Desaturation via Magnetorquer-Reference-Cited by-同舟云学术

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Spacecraft Attitude Control using NSTSM and RW Desaturation via Magnetorquer

Published:2022-12-14 Issue: Volume: Page:
ISSN:
Container-title:2022 Eighth Indian Control Conference (ICC)
language:
Short-container-title:

Author:

Saini Vikram Kumar¹,Giri Dipak Kumar²

Affiliation:

1. Indian Institute of Technology Kanpur,PhD student in Flight Mechanics and Control, Department of Aerospace Engineering,India,208016

2. Indian Institute of Technology Kanpur,Faculty member in Flight Mechanics and Control, Department of Aerospace Engineering,India,208016

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10093231/10093251/10093376.pdf?arnumber=10093376

Reference10 articles.

1. Spacecraft Attitude and Reaction Wheel Desaturation Combined Control Method

2. Reaction Wheels Desaturation Using Magnetorquers and Static Input Allocation

3. Magnetocoulombic Attitude Control of Earth-Pointing Satellites

4. Optimal Combined Reaction-Wheel Momentum Management for Earth-Pointing Satellites

5. Three-axis Attitude Control with Two Reaction Wheels and Magnetic Torquer Bars

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