Guaranteed Cost Controller Design of Spacecraft Wide Angle Attitude Maneuver Based on Sum-of-squares Optimization

CAI  Zongping; CHEN  Qi; MA  Qingliang; CAO  Chuangfeng; YIN  Xiaojing

doi:10.15892/j.cnki.djzdxb.2013.01.015

CAI Zongping, CHEN Qi, MA Qingliang, CAO Chuangfeng, YIN Xiaojing

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2013, Vol. 33 ›› Issue (1) : 39-43.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2013, Vol. 33 ›› Issue (1) : 39-43. DOI: 10.15892/j.cnki.djzdxb.2013.01.015

MISSILES AND GUIDANCE TECHNOLOGY

Guaranteed Cost Controller Design of Spacecraft Wide Angle Attitude Maneuver Based on Sum-of-squares Optimization

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2013, 33(1): 39-43 https://doi.org/10.15892/j.cnki.djzdxb.2013.01.015

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Received	Published
2012-05-14	2013-02-20
Issue Date
2025-05-24

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