Application of hybrid robust three-axis attitude control approach to overactuated spacecraft—A quaternion based model
Author:
Publisher
Springer Science and Business Media LLC
Subject
Metals and Alloys,General Engineering
Link
http://link.springer.com/content/pdf/10.1007/s11771-016-3228-4.pdf
Reference40 articles.
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3. LU Kun-feng, XIA Yuan-qing, FU Meng-yin. Controller design for rigid spacecraft attitude tracking with actuator saturation [J]. Information Sciences, 2013, 220: 343–366.
4. PUKDEBOON C, ZINOBER A S I. Control Lyapunov function optimal sliding mode controllers for attitude tracking of spacecraft [J]. Journal of the Franklin Institute, 2012, 349(2): 456–475.
5. MAZINAN A H, PASAND M, SOLTANI B. Full quaternion based finite-time cascade attitude control approach via pulse modulation synthesis for a spacecraft [J]. ISA Transactions, 2015, 58: 567–585.
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