A Trajectory Estimation Method for Complex Maneuverable Aircraft Based on Learnable Extended Kalman Filter
A technology that extends Kalman and aircraft, applied in the field of information calculation based on knowledge and models, can solve the problem of low precision, achieve the effect of simplifying parameter adjustment and improving the accuracy of track estimation
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[0059] The learnable extended Kalman filter method for complex maneuvering target track estimation described in this embodiment is implemented according to the following steps:
[0060] Step 1: Build a maneuver model of the target
[0061] Assuming that the earth is a true sphere, ignoring the rotation, the three-dimensional dynamic model of the aircraft is obtained:
[0062]
[0063] Among them, r is the distance from the center of mass of the aircraft to the center of the earth, θ is the longitude, φ is the latitude, v is the velocity, γ is the ballistic inclination, ψ is the ballistic declination, m is the mass of the aircraft, R e =6,378,135m is the radius of the earth, g 0 is the acceleration of gravity, S ref is the characteristic area of the aircraft, ρ=ρ 0 e -βh is the atmospheric density, and is the lift coefficient and drag coefficient when the lift-drag ratio of the aircraft is the largest, c l is the normalized lift coefficient, and σ is the roll angl...
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