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Research on Attitude Control Under Wide-Envelope for Flying-Wing UAVs Combining Tracking Differentiator and Incremental Nonlinear Dynamic In-version
陈清阳 贾政敏 鲁亚飞 王玉杰 王鹏
Acta Aeronautica et Astronautica Sinica . 0, (): 1 -0 .  DOI: 10.7527/S1000-6893.2026.33119

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Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics

All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341