System and method for vehicle positioning and orientation aiming with fusion of inertia and satellite
A satellite positioning, positioning and orientation technology, which is applied in satellite radio beacon positioning systems, radio wave measurement systems, measuring devices, etc., can solve problems such as poor reliability and poor positioning accuracy, and achieve improved accuracy and reliability, and high-precision positioning And directional function, high reliability positioning and directional effect
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Embodiment 1
[0050] like Figures 1 to 3 As shown, the present invention discloses a vehicle-mounted positioning and orientation targeting system that integrates inertia and satellites. The system mainly includes inertial positioning and orientation equipment and satellite positioning and orientation equipment. The inertial positioning and orientation equipment mainly includes laser strapdown inertial groups, autocollimation light Tube, barometric altimeter, Hall odometer, dead reckoning unit, extended Kalman filter, standard Kalman filter, joint Kalman filter and cable network for signal transmission, satellite positioning and orientation equipment mainly includes main antenna, Auxiliary antenna, satellite positioning and orientation host, optical measurement combination unit and target light source generation device; among them, the optical measurement combination unit and target light source generation device together form an optical reference transmission subsystem, which completes the ...
Embodiment 2
[0067] This embodiment is based on the same inventive concept as Embodiment 1, such as Figure 1-3 As shown, this embodiment specifically discloses a method for merging inertial and satellite-based vehicle positioning and targeting, or in other words, this embodiment actually discloses a method for aiming using fused inertial and satellite-based vehicle positioning and directional targeting. The method includes the following steps.
[0068] In the inertial orientation data acquisition step, the autonomous inertial orientation is completed through the laser strapdown inertial group, and the inertial orientation data is generated; in this embodiment, this step also includes the step of temperature compensation for the inertial devices in the laser strapdown inertial group. In this embodiment, temperature-related error compensation is performed on the laser gyroscope and accelerometer, and the continuous compensation model can be used to improve the compensation accuracy, so as t...
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