A sun sensor processing chip determination method with multiple configuration functions

A solar sensor and processing chip technology, applied in instruments, simulators, computer control, etc., can solve the problems of small size and high system integration, and achieve the effect of reduced chip size, easy engineering technology, and good achievability

Active Publication Date: 2017-02-01
BEIJING INST OF CONTROL ENG
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

Existing solar sensors cannot meet the development requirements of current satellites in terms of size, weight and power consumption. Therefore, solar sensors need to be developed with low power consumption, small size and high system integration.

Method used

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  • A sun sensor processing chip determination method with multiple configuration functions
  • A sun sensor processing chip determination method with multiple configuration functions
  • A sun sensor processing chip determination method with multiple configuration functions

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Experimental program
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Embodiment Construction

[0058] The concrete realization thought of the present invention is: design a kind of sun sensor special-purpose processing chip with multiple configuration functions, carry out with 150K anti-radiation reinforcement mother chip, adopt CMOS 0.5um process to realize physical design, through the chip function, the number of pins And the evaluation of pin driving ability, this dedicated processing chip adopts the small package solution of QFP64.

[0059] The concrete realization process of the present invention is as figure 1 As shown, the specific steps are:

[0060] (1) Determine the pin position of the sun sensor probe type interface on the chip to be determined and the method for judging the type of probe; the type of probe includes analog type, "0-1" type and digital type.

[0061] The method for judging the type of the probe is specifically:

[0062] Before confirming that the chip is powered on, if the sun sensor probe is a digital probe, fix the level of the sun sensor ...

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Abstract

Provided is a sun sensor processing chip determination method possessing various configuration functions. The method comprises the following steps that function design verification of a sun sensor dedicated processing chip is performed; the input and output port of the sun sensor dedicated processing chip is constrained so that integrated analysis and front end design verification are realized; a 150K anti-radiation reinforcing master slice is processed, physical design is realized by adopting a CMOS0.5 mu m technology, and rear end time sequence verification is performed; and the chip functions, the number of pins and pin driving capacity are analyzed, and the packaging scheme of the sun sensor dedicated processing chip is designed and implemented. The design adopts a UART communication unit with high reliability, adopts a three-mode redundancy technology with respect to important data, and possesses the flexible configuration functions of UART communication protocols, sun sensor probe types and different obits of digital sun sensor view field monitoring code thresholds so that the requirements of different orbit satellites can be met.

Description

technical field [0001] The invention relates to a method for determining a solar sensor processing chip, in particular to a method for determining a solar sensor processing chip with multiple configuration functions, which is suitable for highly integrated and miniaturized solar sensor circuits; and belongs to the field of chip design . Background technique [0002] The sun sensor is a commonly used attitude sensor in space missions, which is used to measure the incident angle of the sun relative to the sun sensor on the spacecraft. Almost all spacecraft need to be equipped with sun sensors in order to complete the attitude control tasks of the spacecraft at various stages according to the attitude feedback information provided by the sun sensors. [0003] At present, three types of solar sensor probes, digital, analog and "0-1" are most commonly used in spacecraft. Among them, the digital sun sensor probe is used to measure the orientation of the sun and the orientation o...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B19/042
CPCG05B19/042
Inventor 赵媛彭斌贾靳莫亚男吕政欣
Owner BEIJING INST OF CONTROL ENG
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