aluminum etch

**Aluminum Metal Etch Mathematical Modeling** 1. Overview 1.1 Why Aluminum Etch Modeling is Complex Aluminum etching (typically using $\text{Cl}_2/\text{BCl}_3$ plasmas) involves multiple coupled physical and chemical phenomena: - Plasma generation and transport → determines species fluxes to wafer - Ion-surface interactions → physical and chemical mechanisms - Surface reactions → Langmuir-Hinshelwood kinetics - Feature-scale evolution → profile development inside trenches/vias - Redeposition and passivation → sidewall chemistry 1.2 Fundamental Reaction The basic aluminum chlorination reaction: $$ \text{Al} + 3\text{Cl} \rightarrow \text{AlCl}_3 \uparrow $$ Complications requiring sophisticated modeling: - Breaking through native $\text{Al}_2\text{O}_3$ layer (15-30 Å) - Maintaining profile anisotropy - Controlling selectivity to mask and underlayers - Managing Cu residues in Al-Cu alloys 2. Kinetic and Chemical Rate Modeling 2.1 General Etch Rate Formulation A comprehensive etch rate model combines three primary mechanisms: $$ ER = \underbrace{k_{th} \cdot \Gamma_{Cl} \cdot f(\theta)}_{\text{thermal chemical}} + \underbrace{Y_s \cdot \Gamma_{ion} \cdot \sqrt{E_{ion}}}_{\text{physical sputtering}} + \underbrace{\beta \cdot \Gamma_{ion}^a \cdot \Gamma_{Cl}^b \cdot E_{ion}^c}_{\text{ion-enhanced (synergistic)}} $$ Parameter Definitions: | Symbol | Description | Units | |--------|-------------|-------| | $\Gamma_{Cl}$ | Neutral chlorine flux | $\text{cm}^{-2}\text{s}^{-1}$ | | $\Gamma_{ion}$ | Ion flux | $\text{cm}^{-2}\text{s}^{-1}$ | | $E_{ion}$ | Ion energy | eV | | $\theta$ | Surface coverage of reactive species | dimensionless | | $Y_s$ | Physical sputtering yield | atoms/ion | | $\beta$ | Synergy coefficient | varies | | $a, b, c$ | Exponents (typically 0.5-1) | dimensionless | 2.2 Surface Coverage Dynamics The reactive site balance follows Langmuir-Hinshelwood kinetics: $$ \frac{d\theta}{dt} = k_{ads} \cdot \Gamma_{Cl} \cdot (1-\theta) - k_{des} \cdot \theta \cdot \exp\left(-\frac{E_d}{k_B T}\right) - Y_{react}(\theta, E_{ion}) \cdot \Gamma_{ion} \cdot \theta $$ Term-by-term breakdown: - Term 1: $k_{ads} \cdot \Gamma_{Cl} \cdot (1-\theta)$ — Adsorption rate (proportional to empty sites) - Term 2: $k_{des} \cdot \theta \cdot \exp(-E_d/k_B T)$ — Thermal desorption (Arrhenius) - Term 3: $Y_{react} \cdot \Gamma_{ion} \cdot \theta$ — Ion-induced reaction/removal Steady-State Solution ($d\theta/dt = 0$): $$ \theta_{ss} = \frac{k_{ads} \cdot \Gamma_{Cl}}{k_{ads} \cdot \Gamma_{Cl} + k_{des} \cdot e^{-E_d/k_B T} + Y_{react} \cdot \Gamma_{ion}} $$ 2.3 Temperature Dependence All rate constants follow Arrhenius behavior: $$ k_i(T) = A_i \cdot \exp\left(-\frac{E_{a,i}}{k_B T}\right) $$ Typical activation energies for aluminum etching: - Ion-enhanced reactions: $E_a \approx 0.1 - 0.3 \text{ eV}$ - Purely thermal processes: $E_a \approx 0.5 - 1.0 \text{ eV}$ - Chlorine desorption: $E_d \approx 0.3 - 0.5 \text{ eV}$ 2.4 Complete Etch Rate Expression Combining all terms with explicit dependencies: $$ ER(T, \Gamma_{ion}, \Gamma_{Cl}, E_{ion}) = A_1 e^{-E_1/k_B T} \Gamma_{Cl} \theta + Y_0 \Gamma_{ion} \sqrt{E_{ion}} + A_2 e^{-E_2/k_B T} \Gamma_{ion}^{0.5} \Gamma_{Cl}^{0.5} E_{ion}^{0.5} $$ 3. Ion-Surface Interaction Physics 3.1 Ion Energy Distribution Function (IEDF) For RF-biased electrodes, the IEDF is approximately bimodal: $$ f(E) \propto \frac{1}{\sqrt{|E - E_{dc}|}} \quad \text{for } E_{dc} - E_{rf} < E < E_{dc} + E_{rf} $$ Key parameters: - $E_{dc} = e \cdot V_{dc}$ — DC self-bias energy - $E_{rf} = e \cdot V_{rf}$ — RF amplitude energy - Peak separation: $\Delta E = 2 E_{rf}$ Collisional effects: In collisional sheaths, charge-exchange collisions broaden the distribution: $$ f(E) \propto \exp\left(-\frac{E}{\bar{E}}\right) \cdot \left[1 + \text{erf}\left(\frac{E - E_{dc}}{\sigma_E}\right)\right] $$ 3.2 Ion Angular Distribution Function (IADF) The angular spread is approximately Gaussian: $$ f(\theta) = \frac{1}{\sqrt{2\pi}\sigma_\theta} \exp\left(-\frac{\theta^2}{2\sigma_\theta^2}\right) $$ Angular spread calculation: $$ \sigma_\theta \approx \sqrt{\frac{k_B T_i}{e V_{sheath}}} \approx \arctan\left(\sqrt{\frac{T_i}{V_{sheath}}}\right) $$ Typical values: - Ion temperature: $T_i \approx 0.05 - 0.5 \text{ eV}$ - Sheath voltage: $V_{sheath} \approx 50 - 500 \text{ V}$ - Angular spread: $\sigma_\theta \approx 2° - 5°$ 3.3 Physical Sputtering Yield Yamamura Formula (Angular Dependence) $$ Y(\theta) = Y(0°) \cdot \cos^{-f}(\theta) \cdot \exp\left[b\left(1 - \frac{1}{\cos\theta}\right)\right] $$ Parameters for aluminum: - $f \approx 1.5 - 2.0$ - $b \approx 0.1 - 0.3$ (depends on ion/target mass ratio) - Maximum yield typically at $\theta \approx 60° - 70°$ Sigmund Theory (Energy Dependence) $$ Y(E) = \frac{0.042 \cdot Q \cdot \alpha(M_2/M_1) \cdot S_n(E)}{U_s} $$ Where: - $S_n(E)$ = nuclear stopping power (Thomas-Fermi) - $U_s = 3.4 \text{ eV}$ (surface binding energy for Al) - $Q$ = dimensionless factor ($\approx 1$ for metals) - $\alpha$ = mass-dependent parameter - $M_1, M_2$ = projectile and target masses Nuclear Stopping Power $$ S_n(\epsilon) = \frac{0.5 \ln(1 + 1.2288\epsilon)}{\epsilon + 0.1728\sqrt{\epsilon} + 0.008\epsilon^{0.1504}} $$ With reduced energy: $$ \epsilon = \frac{M_2 E}{(M_1 + M_2) Z_1 Z_2 e^2} \cdot \frac{a_{TF}}{1} $$ 3.4 Ion-Enhanced Etching Yield The total etch yield combines mechanisms: $$ Y_{total} = Y_{physical} + Y_{chemical} + Y_{synergistic} $$ Synergistic enhancement factor: $$ \eta = \frac{Y_{total}}{Y_{physical} + Y_{chemical}} > 1 $$ For Al/Cl₂ systems, $\eta$ can exceed 10 under optimal conditions. 4. Plasma Modeling (Reactor Scale) 4.1 Species Continuity Equations For each species $i$ (electrons, ions, neutrals): $$ \frac{\partial n_i}{\partial t} + abla \cdot \vec{\Gamma}_i = S_i - L_i $$ Flux expressions: - Drift-diffusion: $\vec{\Gamma}_i = -D_i abla n_i + \mu_i n_i \vec{E}$ - Full momentum: $\vec{\Gamma}_i = n_i \vec{v}_i$ with momentum equation Source/sink terms: $$ S_i = \sum_j k_{ij} n_j n_e \quad \text{(ionization, dissociation)} $$ $$ L_i = \sum_j k_{ij}^{loss} n_i n_j \quad \text{(recombination, attachment)} $$ 4.2 Electron Energy Balance $$ \frac{\partial}{\partial t}\left(\frac{3}{2} n_e k_B T_e\right) + abla \cdot \vec{Q}_e = P_{abs} - P_{loss} $$ Heat flux: $$ \vec{Q}_e = \frac{5}{2} k_B T_e \vec{\Gamma}_e - \kappa_e abla T_e $$ Power absorption (ICP): $$ P_{abs} = \frac{1}{2} \text{Re}(\sigma_p) |E|^2 $$ Collisional losses: $$ P_{loss} = \sum_j n_e n_j k_j \varepsilon_j $$ Where $\varepsilon_j$ is the energy loss per collision event $j$. 4.3 Plasma Conductivity $$ \sigma_p = \frac{n_e e^2}{m_e( u_m + i\omega)} $$ Skin depth: $$ \delta = \sqrt{\frac{2}{\omega \mu_0 \text{Re}(\sigma_p)}} $$ 4.4 Electromagnetic Field Equations Maxwell's equations (frequency domain): $$ abla \times \vec{E} = -i\omega \vec{B} $$ $$ abla \times \vec{B} = \mu_0 \sigma_p \vec{E} + i\omega \mu_0 \epsilon_0 \vec{E} $$ Wave equation: $$ abla^2 \vec{E} + \left(\frac{\omega^2}{c^2} - i\omega\mu_0\sigma_p\right)\vec{E} = 0 $$ 4.5 Sheath Physics Child-Langmuir Law (Collisionless Sheath) $$ J_{ion} = \frac{4\epsilon_0}{9}\sqrt{\frac{2e}{M}} \cdot \frac{V_s^{3/2}}{s^2} $$ Where: - $J_{ion}$ = ion current density - $V_s$ = sheath voltage - $s$ = sheath thickness - $M$ = ion mass Bohm Criterion Ions must enter sheath with velocity: $$ v_{Bohm} = \sqrt{\frac{k_B T_e}{M}} $$ Ion flux at sheath edge: $$ \Gamma_{ion} = n_s \cdot v_{Bohm} = 0.61 \cdot n_0 \sqrt{\frac{k_B T_e}{M}} $$ Sheath Thickness $$ s \approx \lambda_D \cdot \left(\frac{2 e V_s}{k_B T_e}\right)^{3/4} $$ Debye length: $$ \lambda_D = \sqrt{\frac{\epsilon_0 k_B T_e}{n_e e^2}} $$ 5. Feature-Scale Profile Evolution 5.1 Level Set Method The surface is represented implicitly by $\phi(\vec{r}, t) = 0$: $$ \frac{\partial \phi}{\partial t} + V_n | abla \phi| = 0 $$ Normal velocity calculation: $$ V_n(\vec{r}) = \int_0^{E_{max}} \int_0^{\theta_{max}} Y(E, \theta_{local}) \cdot f_{IEDF}(E) \cdot f_{IADF}(\theta) \cdot \Gamma_{ion}(\vec{r}) \, dE \, d\theta $$ Plus contributions from: - Neutral chemical etching - Redeposition - Surface diffusion 5.2 Hamilton-Jacobi Formulation $$ \frac{\partial \phi}{\partial t} + H( abla \phi, \vec{r}, t) = 0 $$ Hamiltonian for etch: $$ H = V_n \sqrt{\phi_x^2 + \phi_y^2 + \phi_z^2} $$ With $V_n$ dependent on: - Local surface normal: $\hat{n} = - abla\phi / | abla\phi|$ - Local fluxes: $\Gamma(\vec{r})$ - Local angles: $\theta = \arccos(\hat{n} \cdot \hat{z})$ 5.3 Visibility and View Factors Direct Flux The flux reaching a point inside a feature depends on solid angle visibility: $$ \Gamma_{direct}(\vec{r}) = \int_{\Omega_{visible}} \Gamma_0 \cdot \cos\theta \cdot \frac{d\Omega}{\pi} $$ Reflected/Reemitted Flux For neutrals with sticking coefficient $s$: $$ \Gamma_{total}(\vec{r}) = \Gamma_{direct}(\vec{r}) + (1-s) \cdot \Gamma_{reflected}(\vec{r}) $$ This leads to coupled integral equations: $$ \Gamma(\vec{r}) = \Gamma_{plasma}(\vec{r}) + (1-s) \int_{S'} K(\vec{r}, \vec{r'}) \Gamma(\vec{r'}) dS' $$ Kernel function: $$ K(\vec{r}, \vec{r'}) = \frac{\cos\theta \cos\theta'}{\pi |\vec{r} - \vec{r'}|^2} \cdot V(\vec{r}, \vec{r'}) $$ Where $V(\vec{r}, \vec{r'})$ is the visibility function (1 if visible, 0 otherwise). 5.4 Aspect Ratio Dependent Etching (ARDE) Empirical model: $$ \frac{ER(AR)}{ER_0} = \frac{1}{1 + (AR/AR_c)^n} $$ Where: - $AR = \text{depth}/\text{width}$ (aspect ratio) - $AR_c$ = critical aspect ratio (process-dependent) - $n \approx 1 - 2$ Knudsen transport model: $$ \Gamma_{neutral}(z) = \Gamma_0 \cdot \frac{W}{W + \alpha \cdot z} $$ Where: - $z$ = feature depth - $W$ = feature width - $\alpha$ = Clausing factor (depends on geometry and sticking) Clausing factor for cylinder: $$ \alpha = \frac{8}{3} \cdot \frac{1 - s}{s} $$ 6. Aluminum-Specific Phenomena 6.1 Native Oxide Breakthrough $\text{Al}_2\text{O}_3$ (15-30 Å native oxide) requires physical sputtering: $$ ER_{oxide} \approx Y_{\text{BCl}_3^+}(E) \cdot \Gamma_{ion} $$ Why BCl₃ is critical: 1. Heavy $\text{BCl}_3^+$ ions provide efficient momentum transfer 2. BCl₃ scavenges oxygen chemically: $$ 2\text{BCl}_3 + \text{Al}_2\text{O}_3 \rightarrow 2\text{AlCl}_3 \uparrow + \text{B}_2\text{O}_3 $$ Breakthrough time: $$ t_{breakthrough} = \frac{d_{oxide}}{ER_{oxide}} = \frac{d_{oxide}}{Y_{BCl_3^+} \cdot \Gamma_{ion}} $$ 6.2 Sidewall Passivation Dynamics Anisotropic profiles require passivation of sidewalls: $$ \frac{d\tau_{pass}}{dt} = R_{dep}(\Gamma_{redeposition}, s_{stick}) - R_{removal}(\Gamma_{ion}, \theta_{sidewall}) $$ Deposition sources: - $\text{AlCl}_x$ redeposition from etch products - Photoresist erosion products (C, H, O, N) - Intentional additives: $\text{N}_2 \rightarrow \text{AlN}$ formation Why sidewalls are protected: At grazing incidence ($\theta \approx 85° - 90°$): - Ion flux geometric factor: $\Gamma_{sidewall} = \Gamma_0 \cdot \cos(90° - \alpha) \approx \Gamma_0 \cdot \sin\alpha$ - For $\alpha = 5°$: $\Gamma_{sidewall} \approx 0.09 \cdot \Gamma_0$ - Sputtering yield at grazing incidence approaches zero - Net passivation accumulates → blocks lateral etching 6.3 Notching and Charging Effects At dielectric interfaces, differential charging causes ion deflection: Surface charge evolution: $$ \frac{d\sigma}{dt} = J_{ion} - J_{electron} $$ Where: - $\sigma$ = surface charge density (C/cm²) - $J_{ion}$ = ion current (always positive) - $J_{electron}$ = electron current (depends on local potential) Local electric field: $$ \vec{E}_{charging} = - abla V_{charging} $$ Laplace equation in feature: $$ abla^2 V = -\frac{\rho}{\epsilon_0} \quad \text{(with } \rho = 0 \text{ in vacuum)} $$ Modified ion trajectory: $$ m \frac{d^2\vec{r}}{dt^2} = e\left(\vec{E}_{sheath} + \vec{E}_{charging}\right) $$ Result: Ions deflect toward charged surfaces → notching at feature bottom. Mitigation strategies: - Pulsed plasmas (allow electron neutralization) - Low-frequency bias (time for charge equilibration) - Conductive underlayers 6.4 Copper Residue Formation (Al-Cu Alloys) Al-Cu alloys (0.5-4% Cu) leave Cu residues because Cu chlorides are less volatile: Volatility comparison: | Species | Sublimation/Boiling Point | |---------|---------------------------| | $\text{AlCl}_3$ | 180°C (sublimes) | | $\text{CuCl}$ | 430°C (sublimes) | | $\text{CuCl}_2$ | 300°C (decomposes) | Residue accumulation rate: $$ \frac{d[\text{Cu}]_{surface}}{dt} = x_{Cu} \cdot ER_{Al} - ER_{Cu} $$ Where: - $x_{Cu}$ = Cu atomic fraction in alloy - At low temperature: $ER_{Cu} \ll x_{Cu} \cdot ER_{Al}$ Solutions: - Elevated substrate temperature ($>$150°C) - Increased BCl₃ fraction - Post-etch treatments 7. Numerical Methods 7.1 Level Set Discretization Upwind Finite Differences Using Hamilton-Jacobi ENO (Essentially Non-Oscillatory) schemes: $$ \phi_i^{n+1} = \phi_i^n - \Delta t \cdot H(\phi_x^-, \phi_x^+, \phi_y^-, \phi_y^+) $$ One-sided derivatives: $$ \phi_x^- = \frac{\phi_i - \phi_{i-1}}{\Delta x}, \quad \phi_x^+ = \frac{\phi_{i+1} - \phi_i}{\Delta x} $$ Godunov flux for $H = V_n | abla\phi|$: $$ H^{Godunov} = \begin{cases} V_n \sqrt{\max(\phi_x^{-,+},0)^2 + \max(\phi_y^{-,+},0)^2} & \text{if } V_n > 0 \\ V_n \sqrt{\max(\phi_x^{+,-},0)^2 + \max(\phi_y^{+,-},0)^2} & \text{if } V_n < 0 \end{cases} $$ Reinitialization Maintain $| abla\phi| = 1$ using: $$ \frac{\partial \phi}{\partial \tau} = \text{sign}(\phi_0)(1 - | abla\phi|) $$ Iterate in pseudo-time $\tau$ until convergence. 7.2 Monte Carlo Feature-Scale Simulation Algorithm: 1. INITIALIZE surface mesh 2. FOR each time step: a. FOR i = 1 to N_particles: - Sample particle from IEDF, IADF - Launch from plasma boundary - TRACE trajectory until surface hit - APPLY reaction probability: * Etch (remove cell) with probability P_etch * Reflect with probability P_reflect * Deposit with probability P_deposit b. UPDATE surface mesh c. CHECK for convergence 3. OUTPUT final profile Variance reduction techniques: - Importance sampling: Weight particles toward features of interest - Particle splitting: Increase statistics in critical regions - Russian roulette: Terminate low-weight particles probabilistically 7.3 Coupled Multi-Scale Modeling | Scale | Domain | Method | Outputs | |-------|--------|--------|---------| | Reactor | m | Fluid/hybrid plasma | $n_e$, $T_e$, species densities | | Sheath | mm | PIC or fluid | IEDF, IADF, fluxes | | Feature | nm-μm | Level set / Monte Carlo | Profile evolution | | Atomistic | Å | MD / DFT | Yields, sticking coefficients | Coupling strategy: $$ \text{Reactor} \xrightarrow{\Gamma_i, f(E), f(\theta)} \text{Feature} \xrightarrow{ER(\vec{r})} \text{Reactor} $$ 7.4 Plasma Solver Discretization Finite element for Poisson's equation: $$ abla \cdot (\epsilon abla V) = -\rho $$ Weak form: $$ \int_\Omega \epsilon abla V \cdot abla w \, d\Omega = \int_\Omega \rho \, w \, d\Omega $$ Finite volume for transport: $$ \frac{d(n_i V_j)}{dt} = -\sum_{faces} \Gamma_i \cdot \hat{n} \cdot A + S_i V_j $$ 8. Process Window and Optimization 8.1 Response Surface Modeling Quadratic response surface: $$ ER = \beta_0 + \sum_{i=1}^{k} \beta_i x_i + \sum_{i=1}^{k} \beta_{ii} x_i^2 + \sum_{i T_i \end{cases} $$ Optimization problem: $$ \max_{\vec{x}} D(\vec{x}) $$ Subject to: - $85° < \text{sidewall angle} < 90°$ - $\text{Selectivity}_{Al:resist} > 3:1$ - $\text{Selectivity}_{Al:TiN} > 10:1$ - $\text{Uniformity} < 3\%$ (1σ) 8.3 Virtual Metrology Prediction model: $$ \vec{y}_{etch} = f_{ML}\left(\vec{x}_{recipe}, \vec{x}_{OES}, \vec{x}_{chamber}\right) $$ Input features: - Recipe: Power, pressure, flows, time - OES: Emission line intensities (e.g., Al 396nm, Cl 837nm) - Chamber: Impedance, temperature, previous wafer history Machine learning approaches: - Neural networks (for complex nonlinear relationships) - Gaussian processes (with uncertainty quantification) - Partial least squares (for high-dimensional, correlated inputs) 8.4 Run-to-Run Control EWMA (Exponentially Weighted Moving Average) controller: $$ \vec{x}_{k+1} = \vec{x}_k + \Lambda G^{-1}(\vec{y}_{target} - \vec{y}_k) $$ Where: - $\Lambda$ = diagonal weighting matrix (0 < λ < 1) - $G$ = process gain matrix ($\partial y / \partial x$) Drift compensation: $$ \vec{x}_{k+1} = \vec{x}_k + \Lambda_1 G^{-1}(\vec{y}_{target} - \vec{y}_k) + \Lambda_2 (\vec{x}_{k} - \vec{x}_{k-1}) $$ 9. Equations: | Physics | Governing Equation | |---------|-------------------| | Etch rate | $ER = k\Gamma_{Cl}\theta + Y\Gamma_{ion}\sqrt{E} + \beta\Gamma_{ion}\Gamma_{Cl}E^c$ | | Surface coverage | $\theta = \dfrac{k_{ads}\Gamma}{k_{ads}\Gamma + k_{des}e^{-E_d/kT} + Y\Gamma_{ion}}$ | | Profile evolution | $\dfrac{\partial\phi}{\partial t} + V_n| abla\phi| = 0$ | | Ion flux (sheath) | $J_{ion} = \dfrac{4\epsilon_0}{9}\sqrt{\dfrac{2e}{M}} \cdot \dfrac{V^{3/2}}{s^2}$ | | ARDE | $\dfrac{ER(AR)}{ER_0} = \dfrac{1}{1 + (AR/AR_c)^n}$ | | View factor | $\Gamma(\vec{r}) = \displaystyle\int_{\Omega} \Gamma_0 \cos\theta \, \dfrac{d\Omega}{\pi}$ | | Sputtering yield | $Y(\theta) = Y_0 \cos^{-f}\theta \cdot \exp\left[b\left(1 - \dfrac{1}{\cos\theta}\right)\right]$ | | Species transport | $\dfrac{\partial n_i}{\partial t} + abla \cdot \vec{\Gamma}_i = S_i - L_i$ | 10. Modern Developments 10.1 Machine Learning Integration Applications: - Yield prediction: Neural networks trained on MD simulation data - Surrogate models: Replace expensive PDE solvers for real-time optimization - Process control: Reinforcement learning for adaptive recipes Example: Gaussian Process for Etch Rate: $$ ER(\vec{x}) \sim \mathcal{GP}\left(m(\vec{x}), k(\vec{x}, \vec{x}')\right) $$ With squared exponential kernel: $$ k(\vec{x}, \vec{x}') = \sigma_f^2 \exp\left(-\frac{|\vec{x} - \vec{x}'|^2}{2\ell^2}\right) $$ 10.2 Atomistic-Continuum Bridging ReaxFF molecular dynamics: - Reactive force fields for Al-Cl-O systems - Calculate fundamental yields and sticking coefficients - Feed into continuum models DFT calculations: - Adsorption energies: $E_{ads} = E_{surface+adsorbate} - E_{surface} - E_{adsorbate}$ - Activation barriers via NEB (Nudged Elastic Band) - Electronic structure effects on reactivity 10.3 Digital Twins Components: - Real-time sensor data ingestion - Physics-based + ML hybrid models - Predictive maintenance algorithms - Virtual process development Update equation: $$ \vec{\theta}_{model}^{(k+1)} = \vec{\theta}_{model}^{(k)} + K_k \left(\vec{y}_{measured} - \vec{y}_{predicted}\right) $$ 10.4 Uncertainty Quantification Bayesian calibration: $$ p(\vec{\theta}|\vec{y}) \propto p(\vec{y}|\vec{\theta}) \cdot p(\vec{\theta}) $$ Propagation through models: $$ \text{Var}(y) \approx \sum_i \left(\frac{\partial y}{\partial \theta_i}\right)^2 \text{Var}(\theta_i) $$ Monte Carlo uncertainty: $$ \bar{y} \pm t_{\alpha/2} \cdot \frac{s}{\sqrt{N}} $$ Physical Constants | Constant | Symbol | Value | |----------|--------|-------| | Boltzmann constant | $k_B$ | $1.381 \times 10^{-23}$ J/K | | Electron charge | $e$ | $1.602 \times 10^{-19}$ C | | Electron mass | $m_e$ | $9.109 \times 10^{-31}$ kg | | Permittivity of vacuum | $\epsilon_0$ | $8.854 \times 10^{-12}$ F/m | | Al atomic mass | $M_{Al}$ | 26.98 amu | | Al surface binding energy | $U_s$ | 3.4 eV | Process Conditions | Parameter | Typical Range | |-----------|---------------| | Pressure | 5-50 mTorr | | Source power (ICP) | 200-1000 W | | Bias power (RF) | 50-300 W | | Cl₂ flow | 20-100 sccm | | BCl₃ flow | 20-80 sccm | | Temperature | 20-80°C | | Etch rate | 300-800 nm/min |

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