CAPACITIVE SENSING TEQUENIQUES FOR MEMS BASED FORCE FEEDBACK ACCELEROMETER Contents Abstract ………………………………………………………………………………….4 Acknowledgements ……………………………………………………………….5 1. Introduction to chopper stabilization ……………………………. 6 2. system level simulations ………………………………………………….8 2.1 Introduction 8 2.2 Simulink analysis 9 2.3 Introduction of PI 14 3. Circuit design …………………………………………………………………...17 3.1 Introduction 17 1.1. Double ended Op amp 18 1.2. Single ended op amp 20 1.3. Filter 22 1.4. capacitor array 23 4. simulation results ……………………………………………………………..26 5. conclusion …………………………………………………………………………33 5.1 Summary 33 5.2 Scope for future work 33 Appendix ……………………………………………………………………………….34 A Layout 34 2 Microelectronics Lab, Indian Institute of Science. a.1 layout methodolghy 34 a.2 Layout of chip & different parts 35 B Pin configuration 39 C Test plan 42 D Wire Bonding of MEMS Device 44 References …………………………………………………………………………….45 3 Microelectronics Lab, Indian Institute of Science. ABSTRACT For inertial navigation and vibration analysis, MEMS based micro g resolution accelerometers are the best suited choice. In a hybrid solution optimization has to be done at system level. Both mechanical and electronics part of chip has to be designed. This report contains design optimization at system level and then design of electronics part. In mechanical design Displacement amplifying Compliant Mechanism (DaCM) was used to give more capacitance change for given applied force. In electronics design chopper stabilization with boosted gain and correlated double sampling with cross coupled switches to remove common mode noise was used. A new design for achieving high sensitivity by incorporating a Displacement amplifying Compliant Mechanism (DaCM) [15]. In electronics sensing chopper stabilization technique is used to reduce 1/f & offset. One extra opamp stage was introduced which will boost the gain and as it is in nested chopper loop it will not add substantial noise. This enables to get resolution upto 1 part per million of the capacitance. PID controller was also designed and integrated. System level simulations were done in Matlab simulink module and circuit simulation were done in Tanner and Mentor graphics tool kits. The MEMS chip is being fabricated using DRIE process at LEOS. Electronics chip was fabricated using AMIS-0.7µm cmos process 4 Microelectronics Lab, Indian Institute of Science. Acknowledgements I consider myself fortunate to have got opportunity to work under guidance of Dr. Navakanta Bhat. I extend my heartfelt gratitude to him for his guidance, support and encouragement. I would like to thank Prof Ananthasuresh for his helpful discussions and suggestions. I thank my project partners Girish and Manjunath whose research was Springboard for my work. My sincere thanks to Ganesh and Sriram for their kind help during starting stages of this project work. I thank Sandeep, Avanish and Shobi whose help was vital during chip design phase of the project. Finally I thank all members of the Microelectronics lab and friends at IISc for their support and friendship which made my stay at IISc memorable. This project was supported in part by a grant from the Space Technology Cell of IISc-ISRO. This support is gratefully acknowledged. 5 Microelectronics Lab, Indian Institute of Science. 1. Introduction to Chopper stabilization There are many sensing technique used in accelerometer. Switched capacitor[2], correlated double sampling [4][6][7], Unity gain buffer[1] and chopper stabilizations are some of them. Basically these are techniques for reducing the non idealities of the Operational Amplifier (Op Amp). Operational amplifier contains many non idealities such as input offset, 1/f noise, thermal noise [5]. Typically offset ranges to few mV apart from that 1/f noise becomes dominating at low frequency range. Switched capacitance is used to reduce the offset of the op amp. It stores offset on a capacitor and subtracts it from input. This is also known as auto zeroing. Chopper stabilization modulates signal to higher frequency range where there is low 1/f noise then demodulates it to baseband signal after amplification. The reduction in noise is depicted in figure below p p Input Output u y n Modulation Demodulation Signal Noise Noise f 0 f 0 fm f 0 Fig 1 . Chopper Stabilization concept. Here , Chopping frequency is chosen such that Brownian noise instead of 1/f noise will decide the noise floor. At higher frequency the value of 1/f noise keeps on decreasing and at some frequency known as corner frequency it reduces below the Brownian frequency mark. This frequency is generally in 6 Microelectronics Lab, Indian Institute of Science. range of 1 – 2 Mhz. so chopping is done at that frequency.This way baseband noise of the chopper amplifiers is almost equal to Brownian white noise. Offset appears at modulated frequency and its odd harmonics these frequency components need to be removed by subsequent low pass filtering . As shown in figure modulating signal p can take values +1 or -1 , If n is noise signal at low frequency then p 2 = 1 and Output y = (up + n)Ap = uA + A( np). Thus the signal is same but n is multiplied by p. If p has period Tp with duty cycle 50 % , Its Fourier coefficient denoted by Pk is given by . Pk = = Tp 1 Tp ∫ p(t)e - jk(2π / T p ) t dt 0 2 jkπ if k = ± 1, ± 3, ± 5, ..... if k = 0, ± 2, ± 4, ..... = 0 If Sn (ω ) denotes the power spectral density of n , then PSD of pn becomes S pn (ω ) = 4 π 2 ∞ 1 ∑ (2k + 1) k = -∞ 2 Sn (ω - (2k + 1) 2π ) Tp Thus the effect of Sn is strongly reduced in baseband. The circuit realization of chopper stabilization is done by arranging switches at input of amplifier. It can be seen that input is multiplied by +1 & -1 Alternately which is a type of modulation. The output of this circuit is demodulated and filtered to remove offset noise which is at high frequency. Demodulation is done either by using same kind of switching arrangement or by using multiplier circuit. 7 Microelectronics Lab, Indian Institute of Science. 2. System level simulations 2.1 Introduction In a CMOS MEMS device, there is dependence of MEMS device over CMOS circuit & vice a versa. Typically MEMS devices are simulated and optimized in tools which are specific to MEMS analysis like CoventorWare & intelisuite. Which are based on Finite element methods analysis , meshing and Boundary element methods. Where as CMOS part of sensor is simulated in SPICE which mainly solves KCL , KVL based on given node connectivity and device models. There’s no accurate way to simulate both in same platform to see the effect of change in parameters in mechanical domain over electronics circuit & reverse. One of the way is to use electrical equivalent of mechanical structure and then simulate that in SPICE. But in that we have to use a proper scaling factor in order to keep electrical impedance values small [1] for avoiding convergence problem in SPICE. Apart from that full netlist of the circuit has to be ready before hand in order to gain accuracy. Another possibility is to use verilog code to represent all elements in behavioral form and simulate. Matlab can also be used to represent both mechanical & electronics part and simulating full system. Use of simulink models for accelerometers has been done previously [3, 11] . As it gives flexibility to add Matlab code, it has built in tools for signal processing (like decimation filters) and represent of system symbolically making it easy to understand and convey the simulations simulink makes a good choice for system level simulation in CMOS – MEMS. A new design for achieving high sensitivity by incorporating a Displacement amplifying Compliant Mechanism (DaCM) [15]. It was seen the sensitivity of a micro-g high sensitivity accelerometer reported in literature can be improved by around 8 times by adding a DaCM with a slight increase in its natural frequency and negligible change in the fabrication process. This ca easily be reflected in simulink simulations by adding a gain factor. Also equivalent of chopper stabilization can be built showing modulation & demodulation process [16]. 8 Microelectronics Lab, Indian Institute of Science. This chapter describes details of system level simulations carried out. It contain details of both mechanical part (Proof mass , Damper & spring constant system) and electronics part using chopper stabilization. Closed loop analysis with analog feedback , use of PID in feedback and approximate estimation of Kp and Ki values is also explained 2.2 Simulink Analysis Both analog & Digital feedback was investigated using matlab Simulink module for same input parameters and are compared. In simulations input was of 1 mg. Analog Feedback system : The full Block diagram of Analog system is as shown below : Fig 2 Analog Accelerometer model Following is description of each subsystem , Waveforms at different places are also shown. The simulation is carried out assuming input of 1mg Pulse of with 0.2 sec. The Mechanical system is represented as follows 9 Microelectronics Lab, Indian Institute of Science. Fig 3 Mechanical system The Summing point is adding all the forces. As Acceleration is given as input, it is multiplied by the mass of proof mass so as to act as a force quantity. Other forces are The Damping (Proportional to Velocity) and Spring force (Proportional to displacement). Result of this system is Displacement which is measured by the Sensor. Fig 4 Shows Displacement for input of 1mg. for 0.2 sec. applied at time = 0.1 sec. 10 Microelectronics Lab, Indian Institute of Science. Fig 4 Displacement of proof mass The Sensor : Sensor is modeled as follows Fig 5 Sensor Model 11 Microelectronics Lab, Indian Institute of Science. Input for sensor is displacement , Due to displacement there is differential capacitance change between the electrodes. To measure this Capacitance change both electrodes are driven by voltage pulses opposite in polarity but of the same frequency (of around 1 Mhz.). These pulses gets added at the sensor input and output of sensor is modulated wave following the capacitance change. This signal has to be demodulated & that is done by a multiplier. Similar Pulse is multiplied to modulated wave to get a demodulated sense voltage which is direct measure to the capacitance change & hence the acceleration. Figure 6 shows pulse modulated wave proportional to capacitance change Fig 6 Modulated wave Figure 7 shows Sensor output. 12 Microelectronics Lab, Indian Institute of Science. Fig 7 Sensor Output Feedback force : In Analog feedback unlike the digital The feedback is proportional to the sensor output , So a constant factor is multiplied to the sensor output. The constant factor is such that it counters the force applied and tries to bring the proof mass to nominal position. This act as electrical stiffness. All the forces that’s Damping , Stiffness & Electrical feedback Co – exist and act simultaneously on the proof mass. In simulink we can see individual force changing with time and accordingly decide the feedback force. The feedback force acting on proof mass for given input pulse is show below. 13 Microelectronics Lab, Indian Institute of Science. Fig 8 Feedback force 2.3 Introduction of PI Feedback helps in reduction in displacement of proof mass for the same amount of force compared to open loop. But in order to get negligible displacement even when constant force is applied feedback force has to be integrated before being applied to proof mass. This can be done by introducing Proportional – Integral controller in feedback. Finding exact values of Kp & Ki is an iterative method. For tuning PID many method are available to start with better approximated values. One of them is Ziegler-Nichols Step Response Method. Here we get approximate values of Kp & Ki based on open loop step response of the system. Based on this approximate value PID can be fine tuned to meet specific parameters like final displacement of proof mass or the response time. Following is the part of Simulink block diagram added in order to get values of Kp & Ki. 14 Microelectronics Lab, Indian Institute of Science. Fig 9. Simulink block diagram used in finding Kp Ki by Ziegler-Nichols Step Response Method Here, parameters are calculated by taking step response into consideration. This method [8] is based on the approximate model Ga1 (s) . Where ⎛ y ⎞ e − sτ 0 Ga1 ( s ) = ⎜⎜ 0 ⎟⎟ ⎝ τ0 ⎠ s Once this model has been determined by the step response test, we may design controllers according to the following table. Note that only y0 and t0 are used. • y0 = ( y max )(tmax ) − y (tmax ) τ0 = y0 • y max 15 Microelectronics Lab, Indian Institute of Science. Table 1 : Constants for Ziegler-Nichols Step Response Method Controller PI PID Kp 9 10 y0 6 5 y0 Ki 3 10 y0τ 0 3 5 y0τ 0 Kd 0 3τ 0 5 y0 : 16 Microelectronics Lab, Indian Institute of Science. 3. Circuit Design 3.1 Introduction AMIS foundry 0.7µ technology [10] was chosen for fabrication. Circuit simulations were carried out in tanner EDA tools and were verified in mentor graphics. Layout was done in Tanner and Mentor graphics was used in parasitic Capacitance extraction. Layout can be imported in mentor graphics in GDS II format. The block level diagram of the circuit is as shown below Fig 10 : Block diagram of circuit Typically, modulator contained of Transmission gate arrangement which alternately switch ON and OFF. That converts a DC signal to high frequency squire wave. But as here we have a MEMS sensor interface , if we give out of phase pulses to MEMS structure having differential capacitance arrangement we get a modulated output. As shown in fugure below. 17 Microelectronics Lab, Indian Institute of Science. Fig 11 : Modulation using differential capacitors in MEMS device 3.2 Double ended op amp The opamp shown in fig 10 has been realized using Class AB design shown in Fig 12. [9]. This enables large output swing and high slew rate. The designed opamp gives a modest gain of 57 dB. Table2 gives the performance summary of the opamp. Class AB operation was chosen because of its large output current capability. To suppress harmonic distortion single stage amplifier is used. By dynamically biasing the cascade output transistors the amplifier provides large output current and large output voltage range while maintaining gain comparable to alternate single stage design. Table 2 : Op Amp summery Opamp specification Simulated results Supply voltage +5V Open loop gain 57dB Open loop Bandwidth 70kHz Phase margin 52° Slew rate 282.5V/µsec 18 Microelectronics Lab, Indian Institute of Science. Fig 12 : Circuit diagram of differential output Op Amp. The simulation results for gain and phase verses frequency is as follows Fig 13 : Gain Vs Frequency for differential output Opamp 19 Microelectronics Lab, Indian Institute of Science. Fig 14 : Phase Vs Frequency for differential output Opamp 3.3 Single ended op amp A single ended 2 stage op amp with differential input stage and class AB output stage is designed. As its 2 stage op amp proper compensation was used. Opamp was used both in amplification stage and filtering stage. Following is circuit diagram of the amplifier 20 Microelectronics Lab, Indian Institute of Science. Fig 15 : Circuit diagram of single ended op amp. The output characteristic of op amp is as shown below Fig 16 : Gain Vs Frequency for Single ended output Opamp 21 Microelectronics Lab, Indian Institute of Science. Fig 17 : Phase Vs Frequency for Single ended output Opamp 3.4 Filter Fifth order Butterworth filter was used for filtering out high frequency offset from the opamp output so that only low frequency signal is available at the output of filter. The cut off frequency of the filter is used as 2 KHz. It ensures that signal in frequency range of our interest is preserved where as offset which is at high frequency of around 1 Mhz is heavily attenuated. Attenuation at 1 Mhz is around 180 DB. 22 Microelectronics Lab, Indian Institute of Science. Fig 18 : 5th order Butterworth filter All the capacitors are external as their value is very high and they will take lot of on chip area if integrated. Fig 19 : Frequency response of 5th order Butterworth filter 23 Microelectronics Lab, Indian Institute of Science. 3.5 Capacitor Array Accuracy of capacitive sensing suffers due to variations in bond pad capacitance which reduces sensitivity to the sensing capacitance. So a capacitance array is provided to compensate for these variations. This also serves as a on chip test circuit to validate capacitor sensing circuit. Fig 20 : Capacitor bridge Capacitance array can be tuned from 0.5fF to 2pF, which is generally the range of sensing in MEMS sensors [3]. Capacitance values are binary weighted. Latches are provided to hold value of input capacitance and turn on appropriate switch to select that capacitance. There are two such arrays to form a bridge. Each of the arrays can be selected separately and values corresponding to capacitance can be stored in the latches. Capacitance array implementation is shown in Fig 21. Higher values of 24 Microelectronics Lab, Indian Institute of Science. capacitances were implemented using Poly and Metal1 layers. Lower values were implemented using Metal1 - Metal2 layers [10]. In order to reduce parasitic at input of sensing circuit Metal plate of capacitance is chosen as input terminal of sensing circuit and poly as common terminal. Fig 21 Capacitor Array implementation 25 Microelectronics Lab, Indian Institute of Science. 4. Simulation results As shown in block diagram earlier, The input of circuit is modulated wave whose frequency is decided by the input given to the mechanical structure (to the differential capacitance pair). As its in high frequency the 1/f noise is reduced when we use out of phase pulses to sense differential capacitance. The offset of opamp is DC offset and as signal is in high frequency range it is not much affected by the offset. Only the DC value around which pulses are formed will vary not the pulse height which is the indication of signal. The waveform of modulated signal with amplification is as shown below. Fig 22 : Modulated waveform This modulated signal is demodulated using switch arrangement. The switches are transmission gate switches and controlling clock has to be at the same frequency as the of the out of phase pulses applied in the MEMS structure. Demodulated signal contain both low frequency signal and offset which is now in high frequency range. After passing trough one more amplification stage the 26 Microelectronics Lab, Indian Institute of Science. signal is passed trough low pass filter which will remove the offset which is at high frequency and will preserve signal which is in low frequency region. Finally after low pass filtering the output can be fed to PID controller to give proper feedback. The Capacitance verses output voltage plot is shown below. Fig 23 : Ideal C Vs V Output curve As parasitic capacitance is one of the factor which affect the sensitivity of a CMOS – MEMS sensor, Analysis is done with different type of parasitic capacitances. Symmetric parasitic is when both the input terminals see same parasitic capacitances. It was seen that sensitivity of circuit has degraded when the symmetric parasitic are considered at the input. 27 Microelectronics Lab, Indian Institute of Science. Fig 24 : C Vs V Output curve with 100 ppm symmetric parasitic Sensitivity of the sensor is also dependent on its ability to overcome offset in the amplification stage. Offset is generally caused by process variations of the transistor at the input differential pair of op amp. Due to process variation width, length and Vt of the transistor can change, which in tern causes some voltage at output even of both inputs are at same potential. Offset can be introduced purposefully into circuit by changing model files. The value of Vt was changed by 5 % of its value for the transistors pair at the input of amplifier. It was seen after simulations that there is not much effect of offset over the sensitivity of the sensor. 28 Microelectronics Lab, Indian Institute of Science. Fig 25 : C Vs V Output curve with 5 % mismatch in Vt Apart from symmetric parasitic capacitors there’s also possibility that parasitic may be asymmetric. That means one of the pad see more capacitance then other. Asymmetry of 10 ppm and 100 ppm is considered. That means if sense capacitance is 1 pf then 10 af and 100 af asymmetry in parasitic is considered. It was seen that as asymmetry is increased the DC level of the output shifts. That can be explained by considering parasitic capacitance in the capacitor bridge. If parasitic is symmetric bridge can be considered as balanced but it there’s asymmetry there will be some DC offset due to that which will lead to shift in DC level of the signal. It should be noted that if there is considerable asymmetry in parasitics then output may saturate at no load condition. 29 Microelectronics Lab, Indian Institute of Science. Fig 26: C Vs V Output curve with 10 ppm Asymmetry in parasitic 30 Microelectronics Lab, Indian Institute of Science. Fig 27: C Vs V Output curve with 100 ppm Asymmetry in parasitic Lastly, more realistic analysis with both asymmetry as well as offset is done. It is seen that while Asymmetry causes both DC shift and change in sensitivity, Offset have little impact on the output. 31 Microelectronics Lab, Indian Institute of Science. Fig 28: C Vs V Output curve with 100 ppm Asymmetry in parasitic and 5 % mismatch 32 Microelectronics Lab, Indian Institute of Science. 5. Conclusion 5.1 Summary System level simulation of MEMS based accelerometer is done. Analog Closed loop operation of accelerometer with PID controller is studied. Chopper stabilization based Capacitive measurement circuit is designed and fabricated. A resolution of 1ppm of the base capacitance (1pF) is achieved using extra gain stage. The effect of parasitic and dc offset on the sensing circuit to was studied. PID controller with variable Kp & Ki for tuning is designed. Also a amplifier stage providing gain independent of value of Kp is provided. It was observed that in this circuit Parasitic specially asymmetric one affects most to sensitivity compared to symmetric parasitic & offset. The effect of Asymmetric / symmetric parasitic and any bridge asymmetry due to mismatch can be corrected on chip by using the capacitance array. It provides a correction of the range from 0.5fF up to 2pF. This correction can also be used to overcome built in Asymmetry in MEMS devices. 5.2 Scope for Future work Work can be extended further in many ways. Issues like stability in digital feedback can be studied by more accurate modeling in Matlab. Non linear feedback element (Comparator) in digital feedback can be analyzed and proper compensation can be devised. Sensing circuit can be used as front end for closed loop sigma delta feedback. Introduction of comparator in forward and backward loop will make it digital feedback. But care has to be taken that full system is stable. Improvements like using nested chopper stabilization can be done. Optimization of lower frequency Vs ratio of upper to lower frequency can be done. This will help in implementing nested chopper in better way. Also if digital feedback is used options like adding dithering for reduction of noise can be explored. 33 Microelectronics Lab, Indian Institute of Science. Appendix A Layout A.1 Layout Methodology Matching • Common Centroid layout for optimal matching especially in opamp was employed to minimize offset. • Multiple finger layout methodology was employed for wide transistors. Routing • Power and Ground metal lines were made wider to reduce there resistance. • Power rails were distributed evenly across the chip area to reduce power dissipations • Metal 1 and Metal 2 were made wider while routing long paths. • Parallel routing techniques was employed. Pin sharing, placement and general issues. • Input and Output pins were connected proximity to the respective different Blocks. • • Power and ground pins were located diagonally opposite The number of substrate contacts used was high to avoid latch up • Large number of via’s and contacts was used to ensure safe connection 34 Microelectronics Lab, Indian Institute of Science. The layout of the whole chip is shown in fig 29 and the Pin configuration details in Table 3 A.2 Layout of chip & different parts 35 Microelectronics Lab, Indian Institute of Science. Fig 30 : Layout of Chopper stabilisation and PID controller 36 Microelectronics Lab, Indian Institute of Science. Fig 31: Layout of Capacitance array 37 Microelectronics Lab, Indian Institute of Science. Fig 32 : Layout of Latches 38 Microelectronics Lab, Indian Institute of Science. Appendix B Pin Configuration Table 3 Pin configuration (Pins corresponding to Chopper stabilization , Capacitor array , PID controller are shown in bold ) PIN NUMBER I/O PIN DETAILS 1 I VDD 2 I 10nF-pin4 3 I 10nF-Gnd 4 I 10nF-pin2 5 I 10nF-pin6 6 I 10nF-pin5 7 I 10nF-Gnd 8 I 10nF-Gnd 9 O Output 2 10 O Output 1 11 O Output Enable 12 O Out St2 13 I C+ 14 I C0 15 I C- 16 I PID CAPACITOR 1uF-pin17 17 I PID CAPACITOR 1uF-pin16 18 I PID RESISTOR 20K 19 O OUTPUT PID 20 I INPUT PID 21 I D1 (CA) 39 Microelectronics Lab, Indian Institute of Science. 22 I D0 (CA) 23 I D2 (CA) 24 I D3 (CA) 25 I S0 (CA) 26 I S1 (CA) 27 I S2 (CA) 28 I GC 29 I GC+VCO RESISTOR 880K 30 I LOOP FILTER 31 I VCO CAPACITOR 25pF 32 O VCO OUTPUT 33 I GND 34 I FREQUENCY CONTROL 35 O CCO OUTPUT 36 I MEMS SENSOR 37 I CCO RESISTOR 880K 38 O COUNT 0 39 O COUNT 1 40 O COUNT 2 41 O COUNT 3 42 O COUNT 4 43 O COUNT 5 44 O COUNT 6 45 O COUNT 7 46 O OUT + 47 O OUT - 48 O OUTPUT 49 I C+ 50 I C0 40 Microelectronics Lab, Indian Institute of Science. 51 I C- 52 I CLOCK 54 O CLOCK2 55 O CLOCK3 56 O CLOCK4 57 O SCHMITT TRIGGER OUTPUT 58 I CAPACITOR 59 I GAS SENSOR RESISTOR 60 I INPUT VOLTAGE 61 O SCHMITT TRIGGER OUTPUT 62 I SCHMITT TRIGGER INPUT 63 I INPUT (-) 64 I INPUT (+) 41 Microelectronics Lab, Indian Institute of Science. Appendix C Test Plan Power supply voltage: 5V Clock signal: 5V or 6V peak at 1 MHz square wave (50% duty cycle). Components required: Five 10nF capacitance and MEMS based differential Capacitance. Apply 5V between Vdd (Pin 1) to ground (Pin 33) to power up the chip. Clock signal of 5V or 6V peak and 1 MHz frequency needs to be applied at pin 52. Then connect five 10nF base capacitors across pins 2 to 8 these are the filter capacitors. The value of sense capacitance of the MEMS device (or just values of capacitors ) has to be known before hand. Based on that value internal Capacitor bank has to be tuned. This can be done using pin 21 to 27. Four bit value can be fed to latch at a time using pin 21 to 24. The proper nibble can be selected by selecting proper latch using pins 25 & 26. Finally Upper or lower back can be selected by pin 27. Apply 5 V for output enable pin 11 if output of first amplification stage is to be observed. The out of phase modulated and amplified output can be seen on pin 9 & 10. The final low pass filtered output can be seen on pin 12. This output can externally be given to the PID controller input. Asymmetry in the bridge capacitance can be corrected by using the capacitance array. The capacitance array bridge can be tuned to reduce the asymmetry and dc offset in the chip. Finally if 42 Microelectronics Lab, Indian Institute of Science. accelerometer is connected to circuit using wire bonding, the feedback gain can be controlled using proper resistor between pin number 28 & 29. Wire bond a MEMS based differential varactor device that produces differential capacitance change to the capacitive sensing circuit. Tune the bridge capacitance using the capacitance array to ensure the output is not saturated. Measuring the output voltage at pin 46, 47 and 48 can test differential capacitance change produced by the MEMS chip. 43 Microelectronics Lab, Indian Institute of Science. Appendix D Wire Bonding of MEMS Device There are different approaches of realizing electronics in MEMS. One of them is having electronics & MEMS on same die which is fully integrated solution[12]. Other is having two different dies one of which contains MEMS structure and other containing sense electronics[14]. These two dies can be wire bound and packaged as single chip. As very low capacitance measurement is required having two different packages chips is not advisable in this case. Two different packaged chips add on parasitic capacitances significantly and hence should be avoided. Monolithic solution adds processing constrains as same die has to be processed second time without affecting the already processed part of die. Therefore System on Package (SOP) is emerging as the best alternative for MEMS CMOS interface. In SOP solution Once both MEMS & CMOS dies are processed they are to be placed on common hybrid microcircuit (HMC) substrate and they are wire bound. There are multiple ways to wire bond. There can be components on HMC itself. HMC can be designed using CAD or dies can just be pasted on HMC substrate or package & wire bonded to each other & to the pins of packages. In this particular chip if MEMS based accelerometer any other differential capacitance MEMS device is available, It can be interfaced with chip using wire bonding. In that case, Pin 13 & 15 has to be connected to two fixed terminals of the MEMS device. Out of phase pulses has to be applied to the variable terminal (moving mass) of MEMS device and pin 14. Other arrangement remains as mentioned in test plan. Then this assembly is ready for testing. Testing can be done by using a shaker table[4] or a tilt table or by vibrator exciter[13]. Accelerometers are shielded by metal box to avoid RF interference. Sinusoidal excitation is given to the accelerometer of specific frequency and the output of accelerometer is observed on a spectrometer. A spike is observed at given input frequency and at other frequency also some signal is present which is Brownian noise floor white 44 Microelectronics Lab, Indian Institute of Science. in nature. Static testing can be done using a tilt table where accelerometer is tilted by a very small angle which is fraction of degrees which will lead to change in acceleration in range of mG or µg. Output voltage can be measured and checked with simulated value. References [1] Garry K Fedder “Simulation of Micromechanical systems” PhD Dissertation University of California Berkley 1994. [2] Hal& Kulah, Navid Y =dit and Khalil Najafi “ A CMOS Switched-Capacitor Interface Circuit for an Integrated Accelerometer” Pmc. 43rd IEEE Midwest Symp. on Circuits and Systems, Lansing MI, Aug 8-11,2000 [3] Michael Kraft “Closed loop digital accelerometer employing oversampling conversion ” PhD thesis Coventry University 1997. [4] Mark Lemkin, Bernhard E. Boser “A Three-Axis Micromachined Accelerometer with a CMOS Position-Sense Interface and Digital Offset-Trim Electronics” IEEE JOURNAL OF SOLID-STATE CIRCUITS, VOL. 34, NO. 4, APRIL 1999, pp 456- 468. [5] C. Enz et Al “ Circuit techniques for reducing effect of op amp imperfections : Auto zeroing , Correlated double sampling , and Chopper stabilization” Proceedings of IEEE Vol 84 No 11 Nov 1996 [6] Bernhard E Boser and Roger T Howe “Surface Micromachined Accelerometer” IEEE Journal of Solid state Circuits , Vol. 31 No. 3 pp 366 – 75. [7] Naiyavudhi Wongkomet and Bernhard E. Boser “Correlated Double Sampling in Capacitive Position Sensiing Circuits for Micromachined Applications“ [8] Robert A. Paz “ The Design of the PID Controller“ [9] Delta sigma data converters, Theory design and simulations. Steven R. Norsworthy, Richard Schreier, Gaber C. Temes, IEEE Press. [10] Technology engineering CMOS “Electrical parameters CMOS 0.7u C07MA and C07MD” Europractice IMEC, Belgium 45 Microelectronics Lab, Indian Institute of Science. [11] Analog Devices Product introduction http://www.analog.com/accelerometer.html [12] E. Colinet, J. Juillard, S. Guessab, R. Kielbasa “Resolution Enhancement of a Sigma-Delta Micro-Accelerometer using Signal Prediction” International Conference on MEMS, NANO and Smart Systems (ICMENS’04) 2004. [13] Luo, H.; Fedder, G.K.; Carley, L.R. “A 1 mG LATERAL CMOS-MEMS ACCELEROMETER“.The Thirteenth Annual International Conference on Micro Electro Mechanical Systems, 2000. MEMS 2000 [14] KAJITA et al.: “A Two-Chip Interface for a MEMS Accelerometer” IEEE TRANSACTIONS ON INSTRUMENTATION AND MEASUREMENT, VOL. 51, NO. 4, AUGUST 2002 pp 853- 58. [15] Krishnan, G. and Ananthasuresh, G. K., “Objective Evaluation of Displacement-amplifying Compliant Mechanisms for Sensor Applications,” submitted to ASME Design Engineering Technical Conferences, Sep. 2006, Philadelphia, PA. [16] G. Krishnan, C. U. Kshirsagar, B. Manjunatha , N. Bhat and G. K., Ananthasuresh J. John, I. Saha and K. Kanakaraju " Design and System-level Simulation of a High-Resolution Bulk-micromachined Accelerometer with a Displacement-amplifying Compliant Mechanism " Indo-Chinese workshop on MEMS and Related Technologies, New Delhi, INDIA, pp P4-1 – P4-4, Apr. 2006 (Poster paper) 46 Microelectronics Lab, Indian Institute of Science.