CN104142181A - Integrated satellite-borne ultralong linear array infrared detector front end information acquisition circuit - Google Patents

Abstract

The invention discloses an integrated satellite-borne ultralong linear array infrared detector front end information acquisition circuit. Long linear array detector front end signal links are optimized through the circuit, the design method that every eight channels serve as a front end unit module for integration is adopted, and ultralong linear array infrared detector signals can be processed through the multiple front end unit modules; front end analog units are converted into ASIC chips, and each chip can finish the whole process of eight channels of infrared detector signals from analog front ends to digital quantification processing. By the adoption of the technical scheme, design techniques of low noise, a high bandwidth, a high sampling rate, multiple channels, a small size, light weight, low power dissipation, high electromagnetic compatibility and high reliability of satellite-borne ultralong linear array infrared detector front end signals are effectively achieved, the contradiction between an ultralong linear array infrared detector signal acquisition circuit scale and resources of a platform is eliminated, and the technical bottleneck which restricts the development of the satellite-borne infrared remote sensing technology is eliminated.

Description

A kind of integrated spaceborne super long alignment infrared eye front-end information acquisition cuicuit

Technical field

The present invention relates to spaceborne infrared camera technology for information acquisition field, particularly relate to the integrated signal acquisition circuit of a kind of spaceborne infrared long detector array, specifically, a kind of in infrared overlength detector array front-end information is obtained, various requirement (low noise, high bandwidth, high sampling rate, hyperchannel, small size, lightweight, low-power consumption, high electrical-magnetic compatibility, high reliability) is also deposited, and the resource of super long alignment infrared eye signal acquisition circuit scale and platform exists the solution of contradiction.

Background technology

The core devices of modern infrared imaging system is focal plane arrays (FPA) (focal plane array FPA), comprise detector and signal read circuit, and in current spaceborne infrared camera, infrared alignment detector is often no more than 8 output channels, therefore technology for information acquisition is all generally to design by passage, signal condition and Acquisition Circuit that each passage correspondence is complete, tediously long, or adopt analog switch to carry out signal multiplexing before A/D quantizes, the application scenario that this is less in detector scale, residence time is long, sample frequency is low is feasible.But in recent years along with remote sensing technology is in the development of high time, high spatial, high spectral resolution, detector array scale sharply expands, output channel number (tap number) becomes geometric growth, if by existing technical design, increase because signal way becomes multiple, multiplex switch speed, Electro Magnetic Compatibility and noiseproof feature are difficult to meet; On the other hand, the resource requirement meetings such as power consumption, volume, weight are linear to be increased, and satellite platform resource is limited, and this contradiction cannot solve.For example, just there is an above-mentioned difficult problem taking wave detector in the long alignment in MCT4000 × 1 of Shanghai Inst. of Technical Physics, Chinese Academy of Sciences's development as the spaceborne infrared gear of core.

In sum, along with development and the application of spaceborne super long alignment detector, prior art route cannot meet performance index, extensibility extreme difference, and irreconcilable with the resource contradiction of platform, become gradually the bottleneck that the spaceborne infrared remote sensing technology of restriction develops.

Summary of the invention

In order to overcome above-mentioned the deficiencies in the prior art, the invention provides a kind of integrated spaceborne super long alignment infrared eye front-end information acquisition cuicuit, emphasis solves low noise, high bandwidth, high sampling rate, hyperchannel, small size, lightweight, low-power consumption, high scalability, high electrical-magnetic compatibility, the High Reliability Design technical barrier in super long alignment detector front end acquisition of information in spaceborne infrared camera and conditioning.

Technical scheme of the present invention is: front-end information acquisition cuicuit is by polylith front end unit module composition, circuit is optimized long detector array front end signal link, 8 tunnel infrared signal modulate circuits are integrated into 1 front end unit module, and each front end unit module works alone; Adopt multiple front end unit modules to carry out the mode of concurrent working, realize the ability of processing the super long alignment infrared eye signal that reaches units up to ten thousand;

Described front end unit module is carried out integrated to 8 tunnel infrared signal modulate circuits, operational amplifier, sampling holder, high-speed analog switch, high-speed a/d converter, high-speed d/a converter are integrated in a slice asic chip, and an asic chip completes the processing to 2000 yuan of detector 8 tunnel infrared signals.

Specifically comprise the following step:

1) long detector array front end signal link is optimized, adopting every 8 infrared channels is that 1 front end unit module merges integrated mode, processing, SPI interface module, A/D module, D/A module are inputted, subtracted each other, amplify to each front end unit module, mainly containing 8 channel analog signal conditioning module, containing signal;

2) adopt the method for designing based on front end unit module to complete long line series infrared detector acquisition of information, the output signal of 2000 yuan of long line series infrared detectors of each front end unit module energy independent processing;

3) this front end unit module integration is designed to ASIC (dedicated IC chip) curing technology state.

According to the front end unit module of a kind of spaceborne super long alignment infrared eye acquisition of information circuit of the present invention (8 passage infrared signal conditioning ASIC), formed by 24 broadband operational amplifiers in sheet, 1 high-speed a/d, 8 high-speed d/as, employing retainer, high-speed analog switch, 8 PGA, possess following functions:

1) in an infrared eye drives the clock period, can carry out instrumental background signal subtraction, amplification, A/D quantification to 2000 yuan of infrared eyes (8 tunnel output) simulating signal timesharing, channel isolation is greater than 60dB, and signal to noise ratio (S/N ratio) meets 200:1@PGA=31;

2) can pass through spi bus interface, 8 infrared channels are carried out respectively to independently gain-adjusted retaking of a year or grade current state;

3) can pass through D/A, can carry out dynamic background to 8 infrared channel simulating signals and subtract each other;

4) 12 of A/D quantization digits, inversion frequency is not less than 24MSPS, and monolithic output data rate is up to 288Mbps; 12 D/A, inversion frequency is not less than 24MSPS.

Compared with prior art, the invention has the beneficial effects as follows: the scheme of independently carrying out acquisition of information with respect to traditional subchannel, the Integrated design scheme of employing based on front end unit module solved super long alignment detector information comprehensively and obtained the technological difficulties such as low noise in technology, high bandwidth, high sampling rate, hyperchannel, small size, lightweight, low-power consumption, high scalability, high electrical-magnetic compatibility, high reliability, make Chinese spaceborne super long alignment detector information obtain technology and step a stage, opened up a new road in this field.

Specific as follows:

1 power-dissipation-reduced 46%, weight reducing approximately 85%, met the resource constraint of platform to load; Reduce cabling amount, improved EMC ability; Noise, bandwidth, sampling rate, reliability meet system index requirement;

2 extendabilities significantly improve, and the method for employing multi-disc concurrent working can adapt to following detector array and in scale, continue to increase; Compatible super long alignment TDI infrared eye;

3 front-end modules change into after ASIC, have overcome spaceflight apparatus due to distinctive requirement to radioresistance, anti-single particle and device is difficult to the difficulty of type selecting, have improved space loading information obtaining ability.

Brief description of the drawings

Fig. 1 is; Extendible long detector array signal acquisition circuit block diagram.

Fig. 2 is: front end unit module (8 passage infrared signal modulate circuit) structural drawing.

Fig. 3 is: spaceborne 4000 yuan of long line series infrared detector Information Acquisition System schematic diagram.

Fig. 4 is: front end unit module (8 passage infrared signal modulate circuit) internal work sequential chart.

Fig. 5 is: the spaceborne long line series infrared detector acquisition of information circuit pictorial diagram of expanding.

Embodiment

Provide the better embodiment of the present invention below in conjunction with accompanying drawing 3～Fig. 5.

The job step that embodiment 1 obtains system according to the spaceborne 4000 yuan infrared overlength detector array front-end information of Fig. 4 is as follows:

S1, the energising of spaceborne instrument, peripheral drive circuit work, spaceborne 4000 yuan of long line series infrared detectors are exported 32 tunnel simulating signals, send 4 front end unit modules; The in the situation that of the same homophase frequently of input clock, when multiple front end unit module cooperative work, all kinds of synchronizing signals of output must be with frequency homophase, and Phase-offset control is in half master clock cycle;

S2, in the time that detector pixel drives signal CP (accompanying drawing 4) rising edge to arrive, each front end unit module keeps 8 road analog signal samplings of input, correlated-double-sampling subtraction, then sampling keeps;

S3:, the infrared gear background signal from D/A is subtracted each other, expand dynamic range, send A/D to quantize signal by multipath high-speed analog switch, quantization digit is 12bit, inversion frequency is 24MSPS, in driving clock period CP (accompanying drawing 4), infrared eye must complete the A/D conversion (accompanying drawing 4, AD_INT is for converting signal, AD_WR is the output signal after changing) of 8 road signals; Meanwhile, the signal after A/D is quantized, after subsequent process circuit is processed, can feed back to the D/A input end of front end unit module, circular treatment; Also can pass through SPI interface, D/A input end is disconnected and access full 0 signal; In driving the clock period, infrared eye must complete the D/A conversion (accompanying drawing 4, DA_INT is D/A conversion ready signal, DA_WR is data input signal) of data;

S4, according to the A/D data that collect in S3, send instruction and data by SPI interface, regulate the gain of each infrared simulation passage in front end unit module, make to meet the demands.

Claims (1)

1. an integrated spaceborne long line series infrared detector front-end information acquisition cuicuit, it is characterized in that: described front-end information acquisition cuicuit is by polylith front end unit module composition, circuit is optimized long detector array front end signal link, 8 tunnel infrared signal modulate circuits are integrated into 1 front end unit module, and each front end unit module works alone; Adopt multiple front end unit modules to carry out the mode of concurrent working, realize the ability of processing the super long alignment infrared eye signal that reaches units up to ten thousand;

Described front end unit module is carried out integrated to 8 tunnel infrared signal modulate circuits, operational amplifier, sampling holder, high-speed analog switch, high-speed a/d converter, high-speed d/a converter are integrated in a slice asic chip, and an asic chip completes the processing to 2000 yuan of detector 8 tunnel infrared signals.