Single-person positioning navigator and positioning navigation method based on multi-sensor fusion
A multi-sensor fusion, positioning and navigation technology, applied in the field of inertial systems, can solve the problems of inability to achieve indoor positioning and fully autonomous navigation, and achieve the effects of light weight, small size and low cost
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Publication Date
- 2018-09-04
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Figure 1
Abstract
Description
technical field
[0001] The invention relates to inertial navigation and integrated navigation, in particular to a multi-sensor fusion-based single-person positioning navigator and a positioning and navigation method, belonging to the technical field of inertial systems. Background technique
[0002] At present, micro-mechanical (MEMS) technology is quite mature, and it is widely used in various fields of military and civilian, and it is also true in the field of inertia. Due to their small size, low power consumption, light weight and low cost, MEMS gyroscopes and MEMS accelerometers are widely used in the fields of model aircraft, drones, cameras and mobile phones. In addition, sensors such as satellite navigation systems, geomagnetic sensors and barometers are also widely used in car navigation, flight control and other occasions.
[0003] Personal navigation system, PNS (Personal / Pedestrian Navigation System) is mainly used to track and locate the real-time position of w...
Examples
Embodiment Construction
[0017] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.
[0018] see figure 1 , as can be seen from the figure, the present invention is based on a single-person positioning navigator based on multi-sensor fusion, including a global satellite positioning system, a barometer for measuring altitude, a three-axis gyroscope, a three-axis accelerometer and a three-axis geomagnetic sensor, A three-axis gyroscope and a three-axis accelerometer form a micromechanical inertial navigation unit. The attitude angle information obtained by the gyroscope, the position information obtained by the accelerometer, the heading information of the human body provided by the geomagnetic sensor, the altitude information provided by the barometer, and the accelerometer calculate The step frequency information and the position and speed information provided by the global satellite positioning system are input into the Kalma...