The Design of LPV Controller for Spacecraft's Wide Angle Maneuver Based on Square Sum Optimization

CHEN  Qi; CAI  Zongping; MA  Qingliang; YIN  Xiaojing; XU  Chen

doi:10.15892/j.cnki.djzdxb.2012.03.043

CHEN Qi, CAI Zongping, MA Qingliang, YIN Xiaojing, XU Chen

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2012, Vol. 32 ›› Issue (3) : 82-85,95.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2012, Vol. 32 ›› Issue (3) : 82-85,95. DOI: 10.15892/j.cnki.djzdxb.2012.03.043

MISSILES AND GUIDANCE TECHNOLOGY

The Design of LPV Controller for Spacecraft's Wide Angle Maneuver Based on Square Sum Optimization

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2012, 32(3): 82-85,95 https://doi.org/10.15892/j.cnki.djzdxb.2012.03.043

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Received	Published
2011-06-29	2012-06-20
Issue Date
2025-05-29

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