The invention relates to a polarization / inertial navigation integrated navigation method of an embedded unmanned aerial vehicle
kinetic model, which comprises the following steps of: expanding a three-dimensional attitude error angle, a speed error, a
position error, an angular speed error and a
thrust coefficient error of the unmanned aerial vehicle
kinetic model into inertial navigation state parameters as state quantities to form
system state quantities; establishing a
system state equation; taking the course angle calculated by the polarization sensor and the attitude, the speed and the position of the unmanned aerial vehicle
kinetic model as quantity measurement, and establishing a
system measurement equation; establishing a credibility
discrimination function of polarization course measurement based on course angle innovation, and designing a combined navigation
mode switching and
thrust coefficient error feedback strategy; a Kalman filtering method is used for estimating system state quantities, namely an inertial navigation attitude misalignment angle, a speed error and a
position error, and an attitude error angle, a speed error, a
position error and a
thrust coefficient error of an unmanned aerial vehicle dynamic model, so that correction of the attitude and the position of the unmanned aerial vehicle is realized.