Post on 27-Nov-2014
8/5/2004 1
The Antenna Effect: Problem and Solutions
John Liobe
8/5/2004 2
Presentation Outline
• Mechanism of antenna condition• Evolution of the definition of the Antenna
Ratio• Design solutions to antenna violations• Antenna Rule Checks in some common
DRCs• Summary
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Presentation Outline
• Mechanism of antenna condition- Define “antenna”- Describe plasma etching- Examples
• Evolution of the definition of the Antenna Ratio• Design solutions to antenna violations• Antenna Rule Checks in some common DRCs• Summary
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Plasma Induced Damage (PID) = Antenna Effect
• Occurs during manufacturing process• Antennae are floating conduction layers
without shielding layer of oxide [16]-effects poly and metal layers
• The random discharge of the floating node could permanently damage the transistor
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Thin Gate Oxide Damage• Oxide tunneling current (F-N)
introduces more trap states [6] • e- tunnel through the oxide-
semiconductor barrier• e- gather energy and do damage
(break bonds) as they proceed - Due to high electric fields
• Affects gate oxide breakdown and transistor threshold voltages
• Defects enhance this effect• Mechanism is not well
understood
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Damage Characteristics• Different kinds of
indicators for amount of oxide damage
-QBD, breakdown field, and Vth
• PID is proportional to total charge that passes through oxide [13]
• Oxide breakdown is very sensitive to stress polarity [24]
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Plasma Etching• Chips are usually
processed from the bulk up
• Current processes have > 8 layers of interconnect
• Reactive Ion Etching (RIE) -standard method for etching thin films in VLSI manufacturing
• Antenna failures are different for aluminum and copper processes [4]
8/5/2004 Adapted from [2] 8
Example of Antenna Effect
8/5/2004 Adapted from [1] 9
Another Example of Antenna Effect
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Presentation Outline• Mechanism of antenna condition• Evolution of the definition of the
Antenna Ratio- Plasma-based manufacturing processes- Layout dependencies- New antenna model
• Design solutions to antenna violations• Antenna Rule Checks in some common DRCs• Summary
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Three Types of Plasma-based Manufacturing Processes [7]
• Conductor layer pattern etching processes-Amount of accumulated charge is proportional to perimeter length
• Ashing processes-Amount of accumulated charge is proportional to area
• Contact etching processes-Amount of accumulated charge is proportional to area of via
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Classical Definition of Antenna Ratio (AR)
• Ratio of total area and/or perimeter of conducting layer attached to gate to gate area
[15]AR=AreaGateTotal
PerimeterandAreaConductorFloatingExposedTotal
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Extent of the Antenna Effect• Classical theory predicts amount of degradation
is directly proportional to the AR.- charging effect is identical for each metal layer
• However, AR was found to have little or no dependence on antenna effect [12].
• There are also layout dependencies that need to be considered.
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Layout Dependency of Charging Damage
• Extent of charging damage is a function of the geometry that is connected to the gate
- dense-line antennae are more susceptible to PID-electron shading effect
• RIE lag-etch rate differences
• Plasma ashing and oxide deposition
8/5/2004 Adapted from [14] 15
RIE Lag
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New Model of Antenna Effect• Etch time factor needs to be taken into account
[14]
-Q is the total accumulated injected charge into the gate oxide during the etching time
• Better predictor of antenna effect:
[11]
-A is the area of the conducting layer with capacitance C exposed to plasma of current density J-a is the area of the gate with capacitance a exposed to plasma of current density j-α is the capacitance ratio-P is the perimeter of the antenna capacitor-p is the perimeter of the gate capacitor-w is the angular frequency of the plasma power source
gateAQAR =
)()(2
max aApP
cJvv gg αω
πα++
+=
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Observations of PID Based on New Model
• PID has little to no dependence on AR.• Ratio of antenna capacitance to gate
capacitance is good indicator of PID. • PID depends upon the frequency of the
plasma power source.• For oxides <4nm, PID is not particularly
sensitive to stress current• Increasing dielectric constant of gate
without increasing J can decrease PID.
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Presentation Outline
• Mechanism of antenna condition• Evolution of the definition of the Antenna Ratio• Design solutions to antenna violations
-Description of each solution-Comparison of solutions
• Antenna Rule Checks in some common DRCs• Summary
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Design Solutions to Reduce Antenna Effect
Router Options• Break signal wires
and route to upper metal layers by jumper insertion
• All metal being etched is not connected to a gate until the last metal layer is etched
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Design Solutions to Reduce Antenna Effect (cont.)
Dummy transistors• Addition of extra
gates will reduce the capacitance ratio
• Problem of “Reverse “ Antenna Effect [5]
• PFETs more susceptible than NFETs
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Design Solutions to Reduce Antenna Effect (cont.)
Embedded Protection Diode
• Connect reverse-biased diodes to the gate of transistor
• During normal circuit operation, the diode does not affect functionality
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Design Solutions to Reduce Antenna Effect (cont.)
Diode Insertion after placement and route
• Connected of diodes only to those layers with antenna violations
• One diode can be used to protect all input ports that are connected to the same output ports
]1[** NLCost βα +=
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Comparison of Proposed Solutions
Area Overhead Routing Obstruction Performance Degradation
Process Sensitivity
Antenna Reduction
Router Options Worst Severe √ Severe Good
Dummy Transistors Best None None N/A Minimal
Embedded Protection
Diode Insertion
Worse Minimal √ Minimal Better
Diode Insertion after
Placement and Route
Better Minimal √ Minimal Best
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Presentation Outline
• Mechanism of antenna condition• Evolution of the definition of the Antenna Ratio• Design solutions to antenna violations• Antenna Rule Checks in some common
DRCs- Description of antenna rules- Discussion of deficiencies in rules
• Summary
8/5/2004 25
Design Rules for Some Current Technologies – TSMC 0.18um [21]
• Metal antenna ratio is not cumulative• Maximum drawn ratio of field poly perimeter area to the active poly
gate area connected directly to it 200.• When the protection diode is not used, the maximum ratio of each
metal (for M1 to M5) perimeter area to the active Poly gate area400.
• Antenna Ratio = 2[(L+W1)*t]/W2*l-L: floating metal length connected to gate-W1: floating metal width connected to gate-t: metal thickness-W2: connected transistor channel width-l: connected transistor channel length
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Design Rules for Some Current Technologies (cont.) – IBM 0.13um [20]
• Antenna ratio is not cumulative• Poly antennae larger than 100 are NOT
ALLOWED• Floating gate devices with metal antennae
larger than 150 are NOT ALLOWED• Every N-well is required to be tied down by
a N+ diode
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Summary
• PID can have little-no dependence on AR• Ratio of gate capacitance to the antenna
capacitance is a more important PID determinant• PFETs can be more susceptible to PID than
NFETs• Dynamic diode insertion after placement and
route is best technique to reduce antenna effect• Modern CAD tools do not incorporate true
measure of antenna effect
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Outlook• Antenna effect will only become worse!• Risk of yield and reliability excursions still must
by reduced by robust design- Until PID phenomenon is completely understood and eliminated
• The best solution for repairing antenna violations is by hand- Automated methods have serious drawbacks - Fastest and most accurate manual implementation is with useful information
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References• [1] L.-D. Huang et al., “A Polynomial Time-Optimal Diode Insertion/Routing Algorithm for Fixing Antenna Problem,”
IEEE Transactions on Computer-Aided Design of Integrated Circuits and Systems, Vol. 23, No. 1, pp. 141-147, January 2001.
• [2] H. Shirota, T. Sadakane, M. Terai, and K. Okazaki, “A New Router for Reducing “Antenna Effect” in ASIC Design,” Proceedings of the IEEE Custom Integrated Circuits Conference, pp. 27.5.1-27.5.4, May 1998.
• [3] P.H. Chen, S. Malkani, C.-M. Peng, and J. Lin, “Fixing Antenna Problem by Dynamic Diode Dropping and Jumper Insertion,” Proceedings of the IEEE International Symposium on Quality Electronic Design, pp. 275-283, March 2000.
• [4] A.T. Krishnan, S. Krishnan, and P. Nicollian, “Impact of Gate Area on Plasma Charging Damage: The “Reverse” Antenna Effect,” International Electron Devices Meeting, pp. 20.6.1-20.6.4, December 2002.
• [5] J.F. Chen et al., “Reverse Antenna Effect Due to Process-Induced Quasi-Breakdown of Gate Oxide,” IEEE International Reliability Workshop, pp. 94-97, October 1996.
• [6] Z. Wang, A. Scarpa, C. Salm, and F. Kuper. “Relation between Plasma Process-Induced Failure Fraction and Antenna Ratio,” Proceeding of the International Symposium on Plasma Process-Induced Damage, pp. 16-19, May 2001.
• [7] W. Maly et al., “Design-Manufacturing Interface: Part II – Applications,” Proceedings of the Design, Automation, and Test in Europe, pp. 557-562, February 1998.
• [8] R. Otten, P. Camposano, and P. Groeneveld, “Design Automation for Deepsubmicron: Present and Future,” Proceedings of the Design, Automation, and Test in Europe, pp. 650-657, March 2002.
• [9] S. Krishnan, A. Amerasekera, S. Rangan, and S. Aur, “Antenna Device Reliability for ULSI Processing,” Proceedings of the International Electron Devices Meeting, pp. 21.5.1-21.5.4, December 1998.
• [10] H.T. Heineken et al., “CAD at the Design-Manufacturing Interface,” Proceedings of the Design Automation Conference, pp. 321-326, June 1997.
• [11] D.P. Verret, A. Krishnan, and S. Krishnan, “A New Look at the Antenna Effect,” IEEE Transactions on Electron Devices, Vol. 49, No. 7, pp. 1274-1282, July 2002.
• [12] G.S. Hwang and K.P. Giapis, “On the Dependence of Plasma-Induced Charging Damage on Antenna Area,” Proceedings of the International Symposium on Plasma-Induced Damage, pp. 21-23, May 1999.
• [13] K. Hashimoto, “New Phenomena of Charge Damage in Plasma Etching: Heavy Damage Only through Dense-Line Antenna,” Japanese Journal of Applied Physics, Vol. 32, No. 12B, pp. 6109-6113, December 1993.
• [14] P. Simon, J.-M. Luchies, and W. Maly, “Antenna Ratio Definition for VLSI Circuits,” Proceedings of the International Symposium on Plasma Process-Induced Damage, pp. 16-20, May 1999.
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References (cont.)• [15] Z. Chen and I. Koren, “Layer Reassignment for Antenna Effect Minimization in 3-Layer Channel Routing,”
Proceedings of the IEEE International Symposium on Defect and Fault Tolerance in VLSI Systems, pp. 77-85, November 1996.
• [16] W. Maly, C. Ouyang, S. Ghosh, and S. Maturi, “Detection of an Antenna Effect in VLSI Designs,” Proceedings of the IEEE International Symposium on Defect and Fault Tolerance in VLSI Systems, pp. 86-94, November 1996.
• [17] M. Mardiguian, EMI troubleshooting techniques, McGraw-Hill Publishers, 1999.• [18] K. Kano, Semiconductor Devices, Prentice-Hall, 1998.• [19] http://www.mosis.org/Technical/Designrules/guidelines.html• [20] IBM CMS8SFG Design Manual, 11/25/02.• [21] TSMC 0.18um Design Manual, Document number TA-10A5-4001, pp. 67-68.• [22] http://www.silvaco.com/applicactions/archive/2002/mar2002/mar02_a2/mar02_a2.html• [23] J. Ferguon. “Design-for-Yield,” IEE Electronics Systems and Software, pp. 15-16, June/July 2003. • [24] H.-C. Lin et al., “Characterization of Plasma Charging Damage in Ultrathin Gate Oxides,” IEEE International
Reliability Physics Symposium, pp. 312-317, April 1998.