H∞-PID Controller Design for Missile Autopilot Based on Constrained Particle Swarm Optimization

ZHANG  Min; YING  Qiaopin

doi:10.15892/j.cnki.djzdxb.2016.01.001

H_∞-PID Controller Design for Missile Autopilot Based on Constrained Particle Swarm Optimization

ZHANG Min, YING Qiaopin

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2016, Vol. 36 ›› Issue (1) : 1-4,9.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2016, Vol. 36 ›› Issue (1) : 1-4,9. DOI: 10.15892/j.cnki.djzdxb.2016.01.001

MISSILES AND GUIDANCE TECHNOLOGY

H_∞-PID Controller Design for Missile Autopilot Based on Constrained Particle Swarm Optimization

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2016, 36(1): 1-4,9 https://doi.org/10.15892/j.cnki.djzdxb.2016.01.001

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