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Driving circuit of CCD camera for spaceflight

A driving circuit and resistor technology, which is applied in the field of aerospace CCD cameras, can solve the problems of weak driving ability, large capacitive load, large driving current, narrow working voltage range, weak anti-interference ability, etc., and achieve wide working voltage range and anti-interference Strong ability and good stability

Inactive Publication Date: 2015-05-06
成都市未来合力科技有限责任公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The CCD drive circuit is driven by a programmable logic device, which has the advantages of high integration, good reliability, and easy programming of hardware circuits, but there are still weak drive capabilities that cannot provide large drive current for large capacitive loads, and the operating voltage range is narrow. High static power consumption and weak anti-interference ability

Method used

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  • Driving circuit of CCD camera for spaceflight

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Embodiment Construction

[0009] The present invention will be further described below in conjunction with accompanying drawing:

[0010] The driving circuit of the CCD camera used in spaceflight of the present invention comprises the first capacitor C1, the second capacitor C2, the third capacitor C3, the fourth capacitor C4, the fifth capacitor C5, MAX4426 chip M, the first resistor R1, the second resistor R2, third resistor R3, fourth resistor R4, fifth resistor R5, sixth resistor R6, seventh resistor R7, first diode D1, second diode D2 and DC power supply (not shown in the figure) , the first signal input terminal INA of the MAX4426 chip M is used as the first signal input terminal TM1 of the driving circuit, the second signal input terminal INB of the MAX4426 chip is used as the second signal input terminal TM2 of the driving circuit, and the first terminal of the first capacitor C1 At the same time, it is connected to the positive terminal VDD of the power supply of the MAX4426 chip M and the pos...

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Abstract

The invention discloses a driving circuit of a CCD camera for spaceflight. The driving circuit comprises first to fifth capacitors, an MAX4426 chip, first to seventh resistors, a first diode, a second diode and a DC power supply; the MAX4426 is relatively high in transient response and large current driving capacity; the first capacitor, the second capacitor, the fifth capacitor, the fourth resistor, the fifth resistor and the sixth resistor form a power filtering circuit; the third capacitor, the fourth capacitor, the first diode, the second diode, the first resistor and the second resistor are used for rectifying and stabilizing transient voltage variation of the driving circuit. The driving circuit of the CCD camera for the spaceflight is relatively high in driving capacity, and capable of providing large driving current to the relatively large capacitive load; the increase time and decrease time are matched; the clock offset is small; in addition; the input capacitance is small, the output impedance is small, the working voltage range is wide, the static power consumption is small, the stability is high, and the interference resistance is high.

Description

technical field [0001] The invention relates to a CCD camera for aerospace, in particular to a drive circuit for the CCD camera with high drive capability, high anti-interference capability and low static power consumption. Background technique [0002] With the development of aerospace technology, CCD cameras with high sensitivity and high signal-to-noise ratio have been widely used in the fields of high-precision measurement of spacecraft attitude, space remote sensing, and earth observation. The design of the chip drive circuit is particularly important. The CCD drive circuit is driven by a programmable logic device, which has the advantages of high integration, good reliability, and easy programming of hardware circuits, but there are still weak drive capabilities that cannot provide large drive current for large capacitive loads, and the operating voltage range is narrow. High static power consumption and weak anti-interference ability. Contents of the invention [...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H04N5/369
Inventor 余国灿雍军李海滨
Owner 成都市未来合力科技有限责任公司
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