High Performance Real-time Flight Control Simulation System Design Based on PC Technology

LI  Zhongjian; QIN  Yuanshan

doi:10.15892/j.cnki.djzdxb.2010.02.062

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2010, Vol. 30 ›› Issue (2) : 63-66. DOI: 10.15892/j.cnki.djzdxb.2010.02.062

MISSILES AND GUIDANCE TECHNOLOGY

High Performance Real-time Flight Control Simulation System Design Based on PC Technology

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2010, 30(2): 63-66 https://doi.org/10.15892/j.cnki.djzdxb.2010.02.062

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Received	Published
2009-08-02	2010-04-20
Issue Date
2025-05-28

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