Target detection method, system and equipment based on navigation satellite signals
A technology of navigation satellites and satellite signals, which is applied to satellite radio beacon positioning systems, radio wave measurement systems, measurement devices, etc., can solve the problems of long positioning time and other problems, and achieve the effect of solving long positioning time and fast positioning.
Active Publication Date: 2019-07-23
北京和协航电信息科技有限公司
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[0004] The purpose of the embodiments of the present application is to provide a target detection method, system and equipment based on navigation satellite signals, so as to improve the positioning time deviation existing in the existing missile-borne GPS measurement system in the process of shell target detection in the existing scheme. long question
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[0029] The following will clearly and completely describe the technical solutions in the embodiments of the present application with reference to the accompanying drawings in the embodiments of the present application. Obviously, the described embodiments are only some of the embodiments of the present application, not all of them. The components of the embodiments of the application generally described and illustrated in the figures herein may be arranged and designed in a variety of different configurations. Accordingly, the following detailed description of the embodiments of the application provided in the accompanying drawings is not intended to limit the scope of the claimed application, but merely represents selected embodiments of the application. Based on the embodiments of the present application, all other embodiments obtained by those skilled in the art without making creative efforts belong to the scope of protection of the present application.
[0030] It should ...
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The embodiment of the invention provides a target detection method, a system and equipment based on navigation satellite signals. The target detection method based on navigation satellite signals comprises the following steps that a missile-borne equipment acquires a first original observed quantity of a navigation satellite signal; the missile-borne equipment sends first parameter information carrying a first original observed quantity to the receiving equipment, wherein the first parameter information is used for the receiving equipment to determine the position of a projectile provided withthe missile-borne equipment, so that the receiving equipment can determine the miss distance of the projectile. The missile-borne equipment on the projectile in the embodiments of the application does not need to carry out self-positioning, only needs to send the acquired first original observed quantity to the receiving equipment, and the projectile is positioned by the receiving device, and compared with the missile-borne GPS measuring system in the prior art, the missile-borne equipment on the projectile disclosed by the embodiment of the invention does not need a positioning process, so that quick positioning is realized, and the problem of long positioning time existing in the missile-borne equipment in the prior art is solved.
Description
technical field [0001] The present application relates to the field of shell target detection, in particular, to a target detection method, system and equipment based on navigation satellite signals. Background technique [0002] At present, in the target detection process of the shell, the existing GPS (Global Positioning System, Global Positioning System) measurement system on the shell needs to add ephemeris information before the shell is launched, and after the shell is launched, the bomb-borne equipment on the shell still needs to be added. The process of searching, receiving and positioning is required, that is, the on-board equipment on the shell is required to realize the positioning of the shell, and then send the position of the shell to the receiving device. [0003] However, in the above solution, the positioning of the projectile can only be realized after the missile-borne equipment needs to perform multiple steps. Therefore, the existing missile-borne GPS me...
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Login to View More IPC IPC(8): G01S19/14
CPCG01S19/14
Inventor 杨国军张书义王炎曹士龙庄严高彦钊
Owner 北京和协航电信息科技有限公司