Journal of Projectiles, Rockets, Missiles and Guidance

Decoupling Control Method Based on Incremental Nonlinear Dynamic Inversion for Missiles

CHEN Xingyang, ZHAO Xia, ZHOU Xiaozhi, LI Liang

JPRMG, 2024, 44(2): 76-81. DOI: 10.15892/j.cnki.djzdxb.2024.02.012

Fig.3 Command tracking of attitude response

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