Method for rapidly diagnosing unmanned helicopter sensor faults
A sensor failure, unmanned helicopter technology, applied in the direction of instruments, special data processing applications, electrical digital data processing, etc., to achieve the effect of low false alarm rate and false alarm rate
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[0022] In order to further clarify the present invention in detail, the following describes in detail in conjunction with the accompanying drawings and preferred embodiments.
[0023] Usually, as figure 1 As shown, the controller (1) and the sensor (3) set on the unmanned helicopter (2) are used as the linear steady-state flight control system of the unmanned helicopter (2), which can be described by the following state space model.
[0024] (1)
[0025] In the formula, is the state vector; is the control vector; is the observation vector (or the output vector of the sensor), , , is a constant matrix of the corresponding dimension.
[0026] When the system fails, the above model will change accordingly. Generally, sensor fault types include stuck, gain change, constant deviation and other fault types. The above sensor fault behavior will affect the dynamic performance of the closed-loop feedback system, so it is necessary to perform fault diagnosis and fault-...
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