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Inverted VLBI deep space unidirectional navigation positioning method

A navigation positioning and deep space technology, applied in the field of deep space navigation, can solve problems such as non-convergence, poor timeliness of two-way navigation in deep space, excessive DOP iterations, etc., to reduce dependence, have real-time and autonomy, and solve timeliness poor sex effect

Active Publication Date: 2018-03-09
XIAN INSTITUE OF SPACE RADIO TECH
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Problems solved by technology

This method uses the baseline information of multiple deep space stations to solve the problem of non-convergent iterations and inability to solve the problem caused by excessive DOP when performing long-distance positioning based on the one-way ranging system, and solves the problem of poor timeliness of two-way navigation in deep space. The problem

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  • Inverted VLBI deep space unidirectional navigation positioning method
  • Inverted VLBI deep space unidirectional navigation positioning method
  • Inverted VLBI deep space unidirectional navigation positioning method

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Embodiment Construction

[0067] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be described in further detail below with reference to the accompanying drawings.

[0068] Such as figure 1 As shown, the method of the present invention requires more than three deep space stations to broadcast uplink signals, and the following three deep space stations are used as examples to specifically illustrate the specific implementation steps of using the system of the present invention to carry out navigation and positioning of deep space detectors:

[0069] Step 1. Unify the space-time references of deep space detectors and multiple ground deep space stations.

[0070] The time reference of the unified deep space probe and multiple ground deep space stations is UTC time, and the space reference is in the earth-centered earth-fixed coordinate system.

[0071] Step 2, synchronize the clocks between multiple ground-based deep space station...

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Abstract

The invention provides an inverted VLBI deep space unidirectional navigation positioning method. By the advantages of improvement of deep space distance measurement and speed measurement precision ofa deep space atomic clock as compared with an existing atomic clock, three or more ground deep space station ascending transmitting signals provide navigation positioning service for a deep space detector in a coverage range by a broadcasting mode, the deep space detector receives ascending signals of the more than three deep space stations, base line information among the more than three deep space stations is utilized fully, and on-orbit real-time self-localization is realized by unidirectional inverted VLBI angle measurement and unidirectional ascending range measurement information. The advantages of unidirectional remote distance measurement are achieved by high stability and high accuracy of the deep space atomic clocks to a maximum extent, and dependence of the deep space detector to the ground deep space stations is relieved.

Description

technical field [0001] The invention relates to an inverted VLBI deep space one-way navigation and positioning method, belonging to the technical field of deep space navigation. Background technique [0002] Navigation and positioning of deep space probes is one of the most important technologies in deep space exploration activities. At present, the navigation and positioning of almost all deep space probes rely on two-way radio measurements to obtain the distance and Doppler measurements of the transmitting station and the probe. However, as the distance between the probe and the earth increases, the delay of two-way propagation also increases. The deep space navigation and positioning based on two-way measurement cannot meet the requirements of deep space exploration tasks with high real-time performance. It is the navigation task when the probe or astronaut needs real-time position information to land safely at the destination. Therefore, it is of great value and signif...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C21/24
CPCG01C21/24
Inventor 沈大海蒙艳松雷文英同钊严涛
Owner XIAN INSTITUE OF SPACE RADIO TECH
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