A Method for Intermittent Fault Diagnosis of Aircraft Based on Dual Observers
A fault diagnosis and dual-observer technology, applied in the field of aircraft, can solve problems such as fault isolation and decoupling residuals, and achieve the effects of real-time fault diagnosis, avoiding noise interference, and reducing false alarm rates
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[0051] Such as figure 1 As shown, a dual-observer-based aircraft intermittent fault diagnosis method includes the following steps:
[0052] Step 1: Build an unknown input fault diagnosis observer on the aircraft system model to be diagnosed;
[0053] Consider the dynamic equations for a spacecraft rotating around its center of mass, and only account for gravity, aerodynamic forces, and engine thrust. Take the spacecraft body coordinate system OX b Y b Z b As a moving coordinate system, the dynamic equation for establishing the rotation motion of the spacecraft around the center of mass is:
[0054]
[0055] In the formula, J x 、J y 、J z Respectively, the coordinate system OX of the spacecraft relative to the spacecraft body b Y b Z b The moments of inertia of the three coordinate axes; ω x , ω y , ω z Respectively, the coordinate system OX of the spacecraft relative to the earth-centered inertial coordinate system i Y i Z i The projection components of the ...
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