4 results about "Horizontal coordinate system" patented technology

A kind of compound inertial system attitude simulation test method, compound inertial system obtains launch system initial attitude angle by initial alignment mode;In dynamic loading process, the inertial data of compound inertial system is collected, and the angle signal of attitude simulation platform excitation is synchronously acquired;The attitude of compound inertial system is converted from launch system to local horizontal coordinate system by navigation solution method, while the angle signal of attitude simulation test platform is converted to the attitude angle of local horizontal coordinate system, and relevant operation is carried out, to obtain the dynamic performance parameter of compound inertial system.

A self-calibration method for frame non-orthogonality error and accelerometer error in a dual-axis frame inertial system is proposed. Under static base conditions, the platform is locked at 10 frame angular positions, accelerometer measurements are collected, and the specific force measurement of the inertial system in the platform coordinate system at each locked position is calculated. The attitude matrix of the inertial system from the platform coordinate system to the local horizontal coordinate system at each locked position is also calculated, yielding the acceleration of the inertial system in the local horizontal coordinate system at each locked position, which is used as the error observation. The residuals of the error coefficients are calculated using a total least squares algorithm, and the estimated values ​​of the measured parameters are corrected. Iterative calculations are performed until the iterative convergence criterion is met, obtaining the self-calibration results for each error coefficient. Through the self-calibration and compensation of the error coefficients, the accuracy of attitude measurement of the dual-axis frame inertial system carrier or base affected by the non-orthogonality error of the axis system can be improved.

The application discloses a kind of identification and positioning method and device of aerial visual angle blind area target, belong to computer vision and remote sensing field.The method includes: obtaining the multisensor data of laser radar, camera, IMU and GNSS;Laser radar point cloud is converted to local horizontal coordinate system, and the region with elevation mutation feature is identified as blind area detection candidate area;The specific type and pixel range of aerial visual angle blind area target are identified;The point cloud data corresponding to target mask is extracted, combined with the pose and coordinate information of unmanned aerial vehicle, the three-dimensional coordinates of target under geocentric coordinate system are solved, and the center position is calculated to realize accurate positioning.The technical route of the application is coarse positioning by laser radar point cloud detection candidate area, accurate identification by image semantic segmentation, coordinate mapping solution, solves the problem that existing technology cannot be efficiently identified and positioned, and the accuracy is low, realizes the type identification and high-precision positioning of aerial visual angle blind area target.