Silicon drifting detector processing circuit for X-ray pulsar navigation sensor

A technology for silicon drift detectors and pulsar navigation, which is applied in astronomical navigation, integrated navigators, navigation computing tools, etc. It can solve the problem of not being able to meet the requirements of long-term work of aerospace products, and the inability to use X-ray pulsar navigation sensors, etc. question

Active Publication Date: 2017-03-22
BEIJING INST OF CONTROL ENG
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Problems solved by technology

[0008] Traditional silicon drift detector processing circuits all use commercial or industrial grade components, which cannot meet the long-term work requirements of aerospace products in high-radiation environments, and cannot be used for X-ray pulsar navigation sensors

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  • Silicon drifting detector processing circuit for X-ray pulsar navigation sensor
  • Silicon drifting detector processing circuit for X-ray pulsar navigation sensor
  • Silicon drifting detector processing circuit for X-ray pulsar navigation sensor

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Embodiment Construction

[0049] In the design of the processing circuit of the silicon drift detector, the present invention has carried out technical improvement, adopts anti-radiation aerospace components for design, and satisfies the requirements of aerospace products working for a long time in an orbital high-radiation environment.

[0050] The present invention will be described in further detail below in conjunction with accompanying drawing, as figure 1 As shown, a silicon drift detector processing circuit for an X-ray pulsar navigation sensor of the present invention includes a preamplification module, a reset module and a refrigeration module.

[0051] The pre-amplification module receives the photon signal output by the silicon drift detector, amplifies the signal with low noise and generates a pre-amplified photon signal, which is divided into three outputs: the first output is sent to the pulsar navigation sensor information processing circuit to generate navigation information; the second...

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Abstract

A silicon drifting detector processing circuit for an X-ray pulsar navigation sensor comprises a pre-amplification module, a reset module and a refrigeration module, wherein the pre-amplification module performs low noise amplification on generate pre-amplification photonic signals after receiving photonic signals output by a silicon drifting detector, the pre-amplification photonic signals are output to the pulsar navigation sensor and the reset module respectively, the reset module generates reset signals by the pre-amplification photonic signals and then outputs the reset signals to the silicon drifting detector, the detector is reset, the photonic signals output by the silicon drifting detector are prevented from being saturated, the refrigeration module takes temperature signals of a thermosensitive diode in the detector as input, the temperature is compared with preset temperature, and produced refrigeration current controls the temperature in the detector to be constant with the preset temperature. The detector processing circuit is designed by anti-radiation aerospace class devices, and compared with the prior art, the detector processing circuit can be better suitable for operation on orbit of aerospace products.

Description

technical field [0001] The invention relates to a silicon drift detector processing circuit, in particular to a silicon drift detector processing circuit for X-ray pulsar navigation sensors, which can be used for X-ray pulsar navigation sensors of spacecraft such as satellites and spaceships product. Background technique [0002] The X-ray pulsar navigation sensor conducts navigation according to the pulse signal emitted by the pulsar and the information of the angular position of the pulsar accurately determined in advance. In 1999, the ARGOS advanced research and unconventional stellar characteristics experiment carried on the earth observation satellite launched by the United States initially verified the feasibility of X-ray pulsar navigation. In 2004, the US Defense Advanced Research Projects Agency launched the "X-ray source-based autonomous navigation and positioning" research program. The United States plans to conduct the NICE experiment on the International Space...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C21/02G01C21/20G01C21/24
CPCG01C21/02G01C21/20G01C21/24
Inventor 刘科吕政欣陈建武左富昌梅志武
Owner BEIJING INST OF CONTROL ENG
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