The present invention provides an
avionics device and a
signal processing method based on high-precision inertial navigation, which relate to the field of
aviation navigation control technology. The invention uses environmental complexity assessment to drive
sensor selection, optimizes the acquisition quality of inertial data such as
angular velocity and acceleration, and pixel coordinates, and optical data such as specific data in real time, reduces redundancy, utilizes spectral
decomposition and adaptive filtering, dynamically cleans signals for
environmental noise in different frequency bands, retains key features, uses spatiotemporal feature reconstruction to generate high-dimensional feature vectors, enhances the expressiveness of low-
quality data, dynamically adjusts fusion weights based on
signal-to-
noise ratio and
consistency index, combines predictive error correction to eliminate long-term drift, ensures
processing delay is less than 10ms with hardware support, and maintains
data stability through anti-interference shielding. The invention breaks through the dependence of traditional navigation on external signals, realizes long-term high-precision navigation, is particularly suitable for
aviation covert missions and
civil aviation flights in
severe weather, and improves mission success rate and safety.