Finite Time Convergence Incremental Nonlinear Dynamic Inversion-Based Attitude Control for Flying—Wing Aircraft with Actuator Faults
نویسندگان
چکیده
منابع مشابه
Finite-time fault tolerant attitude control for over-activated spacecraft subject to actuator misalignment and faults
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ژورنال
عنوان ژورنال: Actuators
سال: 2020
ISSN: 2076-0825
DOI: 10.3390/act9030070