Interplanetary autonomous navigation ground test verification system based on information fusion

A technology of pulsars and spacecraft, applied in the direction of integrated navigators, measuring devices, instruments, etc., can solve the problems that the navigation mathematical simulation method cannot adapt to the ground simulation verification of autonomous navigation technology, and the simulation validity is difficult to guarantee, so that the test can be operated Strong, realistic simulation effect, considerate and comprehensive effects

Active Publication Date: 2015-02-11
BEIJING INST OF CONTROL ENG
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Problems solved by technology

[0004] The existing navigation mathematical simulation methods can no longer meet the needs of ground simulation verification of autonomous navigation technology. All signal simulations use mathematical models, and the effectiveness of the simulation is difficult to guarantee. There is an urgent need for sensors with hardware in the loop, high simulation accuracy, and real working conditions. Interstellar autonomous navigation ground test verification system

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  • Interplanetary autonomous navigation ground test verification system based on information fusion

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Embodiment Construction

[0017] Specific embodiments of the present invention will be further described in detail below in conjunction with the accompanying drawings.

[0018] The invention provides a ground test verification system for interstellar autonomous navigation based on information fusion, which is used for ground simulation verification of interstellar autonomous navigation technology, realizes the simulation of the shape and size of navigation celestial bodies, the simulation of X-ray pulsar radiation pulse signals, and enhances The authenticity and reliability of the autonomous interstellar navigation technology ground simulation verification.

[0019] Such as figure 1 Shown is the composition of the system of the present invention, which mainly consists of the following modules: navigation sensor, dynamic celestial body simulator, X-ray pulsar signal simulator, navigation calculation module, sunshade, simulation master control module and mechanical turntable; navigation sensor Installed...

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Abstract

The invention discloses an interplanetary autonomous navigation ground test verification system based on information fusion. The interplanetary autonomous navigation ground test verification system comprises a navigation sensor, a dynamic celestial body simulator, an X-ray pulsar signal simulator, a navigation calculation module, a shading cover, a simulation main control module and a mechanical turntable, wherein the navigation sensor is arranged on the mechanical turntable; the simulation main control module sends an instruction to the navigation calculation module; the navigation calculation module receives the instruction, controls the navigation sensor to image a celestial body image generated by the dynamic celestial body simulator and sends a celestial body imaging result to the navigation calculation module; the navigation calculation module receives the imaging result and then calculates position information of a spacecraft; and furthermore, the navigation calculation module also calculates the position information of the spacecraft according to a received pulse signal of the X-ray pulsar signal simulator and calculates the position information of the spacecraft by an information fusion algorithm. By the interplanetary autonomous navigation ground test verification system, the authenticity and the reliability of ground simulation verification of an autonomous interplanetary navigation technology are improved.

Description

technical field [0001] The invention relates to a ground test verification system for interstellar autonomous navigation based on information fusion, which belongs to the field of physical simulation of interstellar autonomous navigation. Background technique [0002] Interstellar navigation is to determine the orbital information of the spacecraft through sensors, and the navigation of existing spacecraft is mostly completed by ground equipment. With the needs of the development of interstellar exploration of spacecraft, the traditional navigation method relying solely on ground station measurement and control orbit determination will inevitably face problems such as insufficient space-ground communication link capacity and limited measurement distance. Therefore, interstellar autonomous navigation technology has received widespread attention. [0003] The interstellar autonomous navigation technology uses the measurement equipment on the spacecraft to determine the positio...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C25/00G01C21/24
Inventor 王大轶唐强黄翔宇褚永辉熊凯朱志斌
Owner BEIJING INST OF CONTROL ENG
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