A New Approach for Stabilizing Controller Design of Spacecraft Large Angle Attitude Maneuver Based onSum-of-squares Optimization

CHEN  Qi; CAI  Zongping; MA  Qingliang; YIN  Xiaojing

doi:10.15892/j.cnki.djzdxb.2011.06.010

CHEN Qi, CAI Zongping, MA Qingliang, YIN Xiaojing

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2011, Vol. 31 ›› Issue (6) : 47-50.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2011, Vol. 31 ›› Issue (6) : 47-50. DOI: 10.15892/j.cnki.djzdxb.2011.06.010

MISSILES AND GUIDANCE TECHNOLOGY

A New Approach for Stabilizing Controller Design of Spacecraft Large Angle Attitude Maneuver Based onSum-of-squares Optimization

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2011, 31(6): 47-50 https://doi.org/10.15892/j.cnki.djzdxb.2011.06.010

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Received	Published
2011-01-10	2011-12-20
Issue Date
2025-05-30

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