Aircraft attitude fault-tolerant control method based on dynamic control redistribution
A technology of redistribution and dynamic control, applied in attitude control and other directions, which can solve problems such as poor fault-tolerant tracking performance
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[0103] 1. The near-Earth vehicle (NSV) has parameter uncertainties and external disturbances, which can be expressed in the following nonlinear form:
[0104] x · 1 = f 1 ( x 1 ) + g 1 ( x 1 ) x 2 x · 2 = f 2 ...
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