scholarly journals An integrated energy-efficient capacitive sensor digital interface circuit

2014 ◽  
Vol 216 ◽  
pp. 43-51 ◽  
Author(s):  
Hesham Omran ◽  
Muhammad Arsalan ◽  
Khaled N. Salama
Integration ◽  
2017 ◽  
Vol 59 ◽  
pp. 247-254 ◽  
Author(s):  
Zongwei Li ◽  
Xingyin Xiong ◽  
Xiong Liu ◽  
Kedu Han ◽  
Ning Cong ◽  
...  

Micromachines ◽  
2018 ◽  
Vol 9 (12) ◽  
pp. 675 ◽  
Author(s):  
Xiangyu Li ◽  
Jianping Hu ◽  
Xiaowei Liu

Micro-electromechanical system (MEMS) accelerometers are widely used in the inertial navigation and nanosatellites field. A high-performance digital interface circuit for a high-Q MEMS micro-accelerometer is presented in this work. The mechanical noise of the MEMS accelerometer is decreased by the application of a vacuum-packaged sensitive element. The quantization noise in the baseband of the interface circuit is greatly suppressed by a 4th-order loop shaping. The digital output is attained by the interface circuit based on a low-noise front-end charge-amplifier and a 4th-order Sigma-Delta (ΣΔ) modulator. The stability of high-order ΣΔ was studied by the root locus method. The gain of the integrators was reduced by using the proportional scaling technique. The low-noise front-end detection circuit was proposed with the correlated double sampling (CDS) technique to eliminate the 1/f noise and offset. The digital interface circuit was implemented by 0.35 μm complementary metal-oxide-semiconductor (CMOS) technology. The high-performance digital accelerometer system was implemented by double chip integration and the active interface circuit area was about 3.3 mm × 3.5 mm. The high-Q MEMS accelerometer system consumed 10 mW from a single 5 V supply at a sampling frequency of 250 kHz. The micro-accelerometer system could achieve a third harmonic distortion of −98 dB and an average noise floor in low-frequency range of less than −140 dBV; a resolution of 0.48 μg/Hz1/2 (@300 Hz); a bias stability of 18 μg by the Allen variance program in MATLAB.


Author(s):  
Piyush Joshi ◽  
Navin Singhal ◽  
M. Santosh ◽  
Ayan Bandyopadhyay ◽  
Saumya Paliwal ◽  
...  

2014 ◽  
Vol 496-500 ◽  
pp. 1273-1276
Author(s):  
Guo Bao Ding ◽  
Fushan Yao ◽  
Guangxu Ren ◽  
Jie Yu

Based on the theory of electromagnetic compatibility, in view of the automatic loading control system, and carries on the EMC design, analyzed the sensitive circuit part of the principle and method of EMC design, mainly includes the power supply part, CPU control chip, the digital interface circuit and D/A conversion circuit protective measures.


2019 ◽  
Vol 33 (25) ◽  
pp. 1950286
Author(s):  
Fuxiang Huang ◽  
Qiang Fu ◽  
Xiaowei Liu ◽  
Yufeng Zhang ◽  
Zhigang Mao

This paper presents a novel digital silicon gyroscope interface circuit, designed by 0.35 [Formula: see text]m BCD process, and the chip area is 4.8 mm ∗ 5.0 mm. The traditional noise model of charge amplifier decomposes the noise into voltage noise and current noise. But the test results show that current noise accounts for a large proportion, which is not consistent with the theoretical model. Through the analysis of experimental data and the study of operational amplifier’s working principle in charge amplifier, a new noise model is established, which makes the experimental data closer to the theoretical model. The design makes use of the bandpass characteristics of the bandpass sigma–delta modulator consistent with the sensitive structure of the silicon gyroscope, and optimizes the digital principle of the silicon gyroscope. The digital demodulation of bandpass sigma–delta modulator (BP SDM) can directly separate the in-phase component from the orthogonal component, which eliminates the tedious design of carrier signal digitization and multi-digital filtering, simplifies the frame structure of the whole digital silicon gyroscope system and reduces the design difficulty and physical cost. The ASIC of silicon gyroscope digital interface circuit is tested in combination with the sensitive structure. The noise density of 0.0014[Formula: see text]/s/Hz[Formula: see text], zero stability of 1[Formula: see text]/[Formula: see text]h (1[Formula: see text]) and 0.2[Formula: see text]/[Formula: see text]h (Allen variation). The test of ASIC and the whole machine proves the correctness of the theoretical model, which reflects the correctness of the performance of the digital interface circuit of silicon gyroscope.


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