A correctness inspection system for navigation message data of shipborne satellite navigation equipment based on self-calculation
A technology for navigation messages and inspection systems, applied in satellite radio beacon positioning systems, radio wave measurement systems, instruments, etc., can solve problems such as lack of flexibility and dependence on spacecraft data, and achieve the effect of improving efficiency
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Embodiment 1
[0036] like figure 1 As shown, the embodiment of the present application provides a self-calculation-based system for checking the correctness of navigation message data of shipborne satellite navigation equipment, which consists of three application programs: format conversion application 1, data processing application 2, and format recording application 3 Module composition. in:
[0037] Format conversion application program 1 is the interface layer measurement and control data processing program, which is used to realize the processing and conversion functions of navigation messages, measurement elements, and self-positioning data sent by shipborne satellite navigation equipment, and is deployed in the measurement and control unit server, workstation or industrial computer run.
[0038] The data processing application program 2 can be deployed on the same device or a measurement and control unit server, workstation or industrial computer connected to the network to realiz...
Embodiment 2
[0061] The embodiment of the present application provides an algorithm for judging the consistency of satellite positioning errors based on self-calculation. Using the error calculation principle of the satellite positioning system, the self-consistency of each data of the shipborne satellite navigation equipment can be judged at any time, so as to quickly determine the correctness of the navigation message data sent by the equipment. By converting the measurement elements and self-positioning result information that can be provided by the shipborne satellite navigation equipment at any time into the spacecraft navigation data format according to the dimension, the parameters such as satellite orbit and on-planet clock error provided by the ephemeris calculation module, and the almanac are calculated. The ionosphere, troposphere and other correction coefficients provided by the module, the position and pseudo-range parameters in the simulated spacecraft navigation data provided...
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