β : This English translation is in beta — the Traditional-Chinese original is the authoritative version.
The most frequently used formulas, numbers and knobs of the whole site, condensed onto
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Topic Formula Source ISF operational definition Δ ϕ = Γ ( ω 0 τ ) q m a x Δ q \Delta\phi=\dfrac{\Gamma(\omega_0\tau)}{q_{max}}\Delta q Δ ϕ = q ma x Γ ( ω 0 τ ) Δ q [P1] Eq.(10)(11) → impulse_to_phase_shift LTV phase response ϕ ( t ) = 1 q m a x ∫ − ∞ t Γ ( ω 0 τ ) i n ( τ ) d τ \phi(t)=\dfrac{1}{q_{max}}\displaystyle\int_{-\infty}^{t}\Gamma(\omega_0\tau)\,i_n(\tau)\,d\tau ϕ ( t ) = q ma x 1 ∫ − ∞ t Γ ( ω 0 τ ) i n ( τ ) d τ [P1] Eq.(11) → convolution ISF Fourier Γ = c 0 2 + ∑ n c n cos ( n ω 0 τ + θ n ) \Gamma=\dfrac{c_0}{2}+\sum_n c_n\cos(n\omega_0\tau+\theta_n) Γ = 2 c 0 + ∑ n c n cos ( n ω 0 τ + θ n ) [P1] Eq.(12) → fourier Parseval / rms ∑ n = 0 ∞ c n 2 = 2 Γ r m s 2 \sum_{n=0}^\infty c_n^2=2\Gamma_{rms}^2 ∑ n = 0 ∞ c n 2 = 2 Γ r m s 2 [P1] Eq.(20) → rms_isf White noise 1/f² L = 10 log 10 ( Γ r m s 2 q m a x 2 i n 2 ‾ / Δ f 4 Δ ω 2 ) \mathcal{L}=10\log_{10}\!\Big(\dfrac{\Gamma_{rms}^2}{q_{max}^2}\dfrac{\overline{i_n^2}/\Delta f}{4\,\Delta\omega^2}\Big) L = 10 log 10 ( q ma x 2 Γ r m s 2 4 Δ ω 2 i n 2 /Δ f ) [P1] Eq.(21) → white_noise Flicker 1/f³ L = 10 log 10 ( c 0 2 q m a x 2 i n 2 ‾ / Δ f 8 Δ ω 2 ω 1 / f Δ ω ) \mathcal{L}=10\log_{10}\!\Big(\dfrac{c_0^2}{q_{max}^2}\dfrac{\overline{i_n^2}/\Delta f}{8\,\Delta\omega^2}\dfrac{\omega_{1/f}}{\Delta\omega}\Big) L = 10 log 10 ( q ma x 2 c 0 2 8 Δ ω 2 i n 2 /Δ f Δ ω ω 1/ f ) [P1] Eq.(23) → flicker 1/f³ corner Δ ω 1 / f 3 = ω 1 / f c 0 2 2 Γ r m s 2 \Delta\omega_{1/f^3}=\omega_{1/f}\dfrac{c_0^2}{2\Gamma_{rms}^2} Δ ω 1/ f 3 = ω 1/ f 2 Γ r m s 2 c 0 2 [P1] Eq.(24) SSB↔PSD L ( Δ f ) ≈ 1 2 S ϕ ( Δ f ) \mathcal{L}(\Delta f)\approx\tfrac12 S_\phi(\Delta f) L ( Δ f ) ≈ 2 1 S ϕ ( Δ f ) psd phase→time Δ t = Δ ϕ 2 π f 0 \Delta t=\dfrac{\Delta\phi}{2\pi f_0} Δ t = 2 π f 0 Δ ϕ standard rms jitter σ t = 1 2 π f 0 ∫ f 1 f 2 S ϕ d f \sigma_t=\dfrac{1}{2\pi f_0}\sqrt{\displaystyle\int_{f_1}^{f_2}S_\phi\,df} σ t = 2 π f 0 1 ∫ f 1 f 2 S ϕ df serdes Accumulated jitter σ Δ t = κ Δ t \sigma_{\Delta t}=\kappa\sqrt{\Delta t} σ Δ t = κ Δ t , κ = Γ r m s q m a x 1 2 i n 2 ‾ Δ f \kappa=\dfrac{\Gamma_{rms}}{q_{max}}\sqrt{\tfrac12\tfrac{\overline{i_n^2}}{\Delta f}} κ = q ma x Γ r m s 2 1 Δ f i n 2 [P2] Eq.(8)(12) Ring frequency f 0 = 1 2 N τ D f_0=\dfrac{1}{2N\tau_D} f 0 = 2 N τ D 1 [P2] Eq.(15) Ring Γ r m s \Gamma_{rms} Γ r m s Γ r m s = 2 π 2 3 η 3 1 N 1.5 ⇒ Γ r m s ∝ N − 3 / 2 \Gamma_{rms}=\sqrt{\dfrac{2\pi^2}{3\eta^3}}\;\dfrac{1}{N^{1.5}}\Rightarrow\Gamma_{rms}\propto N^{-3/2} Γ r m s = 3 η 3 2 π 2 N 1.5 1 ⇒ Γ r m s ∝ N − 3/2 (at η = 0.75 \eta=0.75 η = 0.75 , ≈ 4 / N 1.5 \approx4/N^{1.5} ≈ 4/ N 1.5 , the solid line in [P2] Fig.8; the radical covers only the constant)[P2] Eq.(16) Ring FOM L = 8 3 η k T P V D D V c h a r ( f 0 Δ f ) 2 \mathcal{L}=\dfrac{8}{3\eta}\dfrac{kT}{P}\dfrac{V_{DD}}{V_{char}}\Big(\dfrac{f_0}{\Delta f}\Big)^2 L = 3 η 8 P k T V c ha r V D D ( Δ f f 0 ) 2 (no N N N !)[P2] Eq.(23) Generalized Adler d θ d t = ( ω 0 − ω i n j ) + Ω ( θ ) \dfrac{d\theta}{dt}=(\omega_0-\omega_{inj})+\Omega(\theta) d t d θ = ( ω 0 − ω inj ) + Ω ( θ ) , Ω = ⟨ Γ ~ i i n j ⟩ \Omega=\langle\tilde\Gamma\,i_{inj}\rangle Ω = ⟨ Γ ~ i inj ⟩ [P3] Eq.(30)(33) APF / amplitude decay τ 0 = 2 Q ω o s c \tau_0=\dfrac{2Q}{\omega_{osc}} τ 0 = ω osc 2 Q , Λ ~ 1 = τ 0 q m a x ∠ 0 ° \tilde\Lambda_1=\dfrac{\tau_0}{q_{max}}\angle0° Λ ~ 1 = q ma x τ 0 ∠0° (in quadrature with the ISF)[P4] Eq.(25)(26)
Canonical numbers (consistent site-wide)
Example Setup Result A: impulse→time q m a x = 1 q_{max}=1 q ma x = 1 pC, Δ q = 1 \Delta q=1 Δ q = 1 fC, Γ = 0.5 \Gamma=0.5 Γ = 0.5 , f 0 = 5 f_0=5 f 0 = 5 GHzΔ ϕ = 5 × 10 − 4 \Delta\phi=5\times10^{-4} Δ ϕ = 5 × 1 0 − 4 rad, Δ t = 15.9 \Delta t=15.9 Δ t = 15.9 fsB: white-noise L \mathcal{L} L Γ r m s = 0.5 \Gamma_{rms}=0.5 Γ r m s = 0.5 , q m a x = 1 q_{max}=1 q ma x = 1 pC, S i = 10 − 24 S_i=10^{-24} S i = 1 0 − 24 A²/Hz, Δ f = 1 \Delta f=1 Δ f = 1 MHzL = − 148 \mathcal{L}=-148 L = − 148 dBc/HzC: jitter integral L ( 1 MHz ) = − 100 \mathcal{L}(1\text{MHz})=-100 L ( 1 MHz ) = − 100 dBc/Hz, 1/f², 1→100 MHz, 5 GHzσ t = 447.9 \sigma_t=447.9 σ t = 447.9 fsRing FOM γ = 2 / 3 \gamma=2/3 γ = 2/3 , V D D / V c h a r = 3 V_{DD}/V_{char}=3 V D D / V c ha r = 3 , P = 1 P=1 P = 1 mW, others as aboveL ≈ − 91 \mathcal{L}\approx-91 L ≈ − 91 dBc/Hz
Want to sweep the parameters yourself? Use the interactive calculator .
Conversion anchors at 5 GHz
1 1 1 mrad ≈ 32 \approx 32 ≈ 32 fs; 1 1 1 rad ≈ 31.8 \approx 31.8 ≈ 31.8 ps; period = 200 =200 = 200 ps.
dBc/Hz → linear: 10 L / 10 10^{\mathcal{L}/10} 1 0 L /10 ; S ϕ = 2 × S_\phi=2\times S ϕ = 2 × linear.
2 × q m a x 2\times q_{max} 2 × q ma x or 1 2 Γ r m s \tfrac12\Gamma_{rms} 2 1 Γ r m s → L \mathcal{L} L drops by 6 dB .
Design knobs (to lower phase noise)
To lower Knob Why 1/f² (white noise) ↑ q m a x q_{max} q ma x (swing/energy), ↓ Γ r m s \Gamma_{rms} Γ r m s L ∝ Γ r m s 2 / q m a x 2 \mathcal{L}\propto\Gamma_{rms}^2/q_{max}^2 L ∝ Γ r m s 2 / q ma x 2 1/f³ (close-in) make the waveform symmetric → ↓ c 0 c_0 c 0 corner ∝ c 0 2 / Γ r m s 2 \propto c_0^2/\Gamma_{rms}^2 ∝ c 0 2 / Γ r m s 2 Jitter (time domain) same as above (same Γ r m s 2 / q m a x 2 \Gamma_{rms}^2/q_{max}^2 Γ r m s 2 / q ma x 2 ); or lock in a PLL/CDR κ ∝ Γ r m s / q m a x \kappa\propto\Gamma_{rms}/q_{max} κ ∝ Γ r m s / q ma x Where noise is injected avoid phases where ∣ Γ ∣ \lvert\Gamma\rvert ∣ Γ ∣ is large (small slope) cyclostationary Γ e f f = Γ α \Gamma_{eff}=\Gamma\alpha Γ e f f = Γ α
v5–v8 quick reference (jitter kernels / κ↔D↔linewidth / App.B / M:N locking / PLL / FOM / SerDes)
Rule for this block: every entry is copied verbatim from its source page, convention flags included. The link is the single source of truth for the derivation.
Kernel Formula (one-sided S ϕ S_\phi S ϕ , ∫ 0 ∞ \int_0^\infty ∫ 0 ∞ convention) White-FM closed form TIE (0th order) σ T I E 2 = 1 ω 0 2 ∫ f 1 f 2 S ϕ d f \sigma_{TIE}^2=\dfrac{1}{\omega_0^2}\displaystyle\int_{f_1}^{f_2}S_\phi\,df σ T I E 2 = ω 0 2 1 ∫ f 1 f 2 S ϕ df — N-period (1st-order difference) σ P 2 ( N ) = 1 ω 0 2 ∫ 0 ∞ S ϕ 4 sin 2 ( π f N T ) d f \sigma_P^2(N)=\dfrac{1}{\omega_0^2}\displaystyle\int_0^\infty S_\phi\,4\sin^2(\pi fNT)\,df σ P 2 ( N ) = ω 0 2 1 ∫ 0 ∞ S ϕ 4 sin 2 ( π f N T ) df = κ 2 N T =\kappa^2NT = κ 2 N T (exact match to [P2] Eq.(8))Cycle-to-cycle (2nd-order difference) σ c 2 c 2 = 1 ω 0 2 ∫ 0 ∞ S ϕ 16 sin 4 ( π f T ) d f \sigma_{c2c}^2=\dfrac{1}{\omega_0^2}\displaystyle\int_0^\infty S_\phi\,16\sin^4(\pi fT)\,df σ c 2 c 2 = ω 0 2 1 ∫ 0 ∞ S ϕ 16 sin 4 ( π f T ) df = 2 κ 2 T ⇒ σ c 2 c = 2 σ P ( 1 ) =2\kappa^2T\Rightarrow\sigma_{c2c}=\sqrt2\,\sigma_P(1) = 2 κ 2 T ⇒ σ c 2 c = 2 σ P ( 1 )
The prefactor is 1 / ω 0 2 1/\omega_0^2 1/ ω 0 2 , not 2 / ω 0 2 2/\omega_0^2 2/ ω 0 2 (that 2 belongs to the double-sided-spectrum or L = 1 2 S ϕ \mathcal{L}=\tfrac12S_\phi L = 2 1 S ϕ bookkeeping).
κ↔D↔linewidth↔ADEV↔S ϕ S_\phi S ϕ dictionary (with the 19.9/39.8 mHz canonical numbers) — diffusion_dictionary
Lead quantity: κ 2 = Γ r m s 2 2 q m a x 2 i n 2 ‾ Δ f \kappa^2=\dfrac{\Gamma_{rms}^2}{2q_{max}^2}\dfrac{\overline{i_n^2}}{\Delta f} κ 2 = 2 q ma x 2 Γ r m s 2 Δ f i n 2 ([P2] Eq.(11)/(12)); canonical (Γ r m s = 0.5 \Gamma_{rms}=0.5 Γ r m s = 0.5 ) gives κ 2 = 0.125 \kappa^2=0.125 κ 2 = 0.125 rad²/s, true LC (Γ r m s = 1 / 2 \Gamma_{rms}=1/\sqrt2 Γ r m s = 1/ 2 ) gives 0.25 0.25 0.25 .
"Outfit" Formula Canonical value κ \kappa κ (phase) / κ t \kappa_t κ t (time)σ Δ ϕ = κ Δ t \sigma_{\Delta\phi}=\kappa\sqrt{\Delta t} σ Δ ϕ = κ Δ t ; κ t = κ / ω 0 \kappa_t=\kappa/\omega_0 κ t = κ / ω 0 κ = 0.354 \kappa=0.354 κ = 0.354 rad/s \sqrt{\text{s}} s D D D convention A / BV a r = D A ∣ t ∣ = 2 D B ∣ t ∣ ⇒ D A = κ 2 , D B = κ 2 / 2 \mathrm{Var}=D_{A}\vert t\vert=2D_{B}\vert t\vert\Rightarrow D_{A}=\kappa^2,\ D_{B}=\kappa^2/2 Var = D A ∣ t ∣ = 2 D B ∣ t ∣ ⇒ D A = κ 2 , D B = κ 2 /2 0.125 0.125 0.125 / 0.0625 0.0625 0.0625 Lorentzian 3-dB linewidth Δ f 3 d B = κ 2 / ( 2 π ) \Delta f_{3\mathrm{dB}}=\kappa^2/(2\pi) Δ f 3 dB = κ 2 / ( 2 π ) 19.9 mHz (true LC 39.8 mHz )S ϕ S_\phi S ϕ coefficient (one-sided)S ϕ = 2 κ 2 / ( 2 π f ) 2 S_\phi=2\kappa^2/(2\pi f)^2 S ϕ = 2 κ 2 / ( 2 π f ) 2 b − 2 = 6.33 × 10 − 3 b_{-2}=6.33\times10^{-3} b − 2 = 6.33 × 1 0 − 3 rad²·HzWhite-FM ADEV σ y ( τ ) = κ / ( 2 π f 0 τ ) \sigma_y(\tau)=\kappa/(2\pi f_0\sqrt\tau) σ y ( τ ) = κ / ( 2 π f 0 τ ) 1.13 × 10 − 11 1.13\times10^{-11} 1.13 × 1 0 − 11 @1s (5 GHz)
Three factor-of-2 families to settle before you convert: one-sided vs double-sided PSD, V a r = D ∣ t ∣ \mathrm{Var}=D\vert t\vert Var = D ∣ t ∣ vs 2 D ∣ t ∣ 2D\vert t\vert 2 D ∣ t ∣ , and SSB / 2 /2 /2 vs / 4 /4 /4 .
Γ r m s 2 = 2 π 2 3 η 3 1 N 3 [ 4 1 + A 3 ( 1 + A ) 3 ] , Γ d c = 2 π η 2 1 N 2 ( 1 − A 1 + A ) , c 0 = 2 Γ d c \Gamma_{rms}^2=\frac{2\pi^2}{3\eta^3}\frac{1}{N^3}\left[4\frac{1+A^3}{(1+A)^3}\right],\quad
\Gamma_{dc}=\frac{2\pi}{\eta^2}\frac{1}{N^2}\left(\frac{1-A}{1+A}\right),\quad c_0=2\Gamma_{dc} Γ r m s 2 = 3 η 3 2 π 2 N 3 1 [ 4 ( 1 + A ) 3 1 + A 3 ] , Γ d c = η 2 2 π N 2 1 ( 1 + A 1 − A ) , c 0 = 2 Γ d c
f 1 / f 3 = f 1 / f ⋅ 3 2 η N ⋅ ( 1 − A ) 2 1 − A + A 2 ( [ P2 ] Eq. ( 52 ) – ( 57 ) , p.803 ) f_{1/f^3}=f_{1/f}\cdot\frac{3}{2\eta N}\cdot\frac{(1-A)^2}{1-A+A^2}\qquad([\text{P2}]\ \text{Eq.}(52)\text{–}(57),\ \text{p.803}) f 1/ f 3 = f 1/ f ⋅ 2 η N 3 ⋅ 1 − A + A 2 ( 1 − A ) 2 ([ P2 ] Eq. ( 52 ) – ( 57 ) , p.803 )
A ≡ f r i s e ′ / f f a l l ′ A\equiv f'_{rise}/f'_{fall} A ≡ f r i se ′ / f f a l l ′ ; A = 1 A=1 A = 1 degenerates exactly to [P2] Eq.(16) (Γ r m s ∝ N − 1.5 \Gamma_{rms}\propto N^{-1.5} Γ r m s ∝ N − 1.5 ); the corner is quadratically flat at A = 1 A=1 A = 1 , symmetric under A → 1 / A A\to1/A A → 1/ A , and ∝ 1 / N \propto1/N ∝ 1/ N . Convention flag: this corner is the [P2] Eq.(7)/(57) value; [P1] Eq.(24) (substituting c 0 = 2 Γ d c c_0=2\Gamma_{dc} c 0 = 2 Γ d c ) = 2 × =2\times = 2 × this value.
Γ ( x ) = f ′ f ′ 2 + f ′ ′ 2 ( [ P1 ] Eq. ( 37 ) , p.193 ) \Gamma(x)=\frac{f'}{f'^{\,2}+f''^{\,2}}\qquad([\text{P1}]\ \text{Eq.}(37),\ \text{p.193}) Γ ( x ) = f ′ 2 + f ′′ 2 f ′ ([ P1 ] Eq. ( 37 ) , p.193 )
Substituting f = cos x f=\cos x f = cos x : the denominator sin 2 + cos 2 = 1 \sin^2+\cos^2=1 sin 2 + cos 2 = 1 , giving Γ = − sin x \Gamma=-\sin x Γ = − sin x exactly, and it stays bounded at the waveform peak (this is what resolves the 1 / slope 1/\text{slope} 1/ slope heuristic's divergence). Ranking of the three methods: A direct impulse injection (most accurate) → B this closed form (one period of waveform suffices) → C slope approximation Γ = f ′ / f m a x ′ 2 \Gamma=f'/f_{max}'^2 Γ = f ′ / f ma x ′2 (cheapest, ring-specific, Eq.(38)).
Injection-locked noise shaping corner = ω L cos θ s s =\omega_L\cos\theta_{ss} = ω L cos θ ss — injection_locking_noise Part A
ω c ≡ ω L cos θ s s = ω L 2 − Δ ω 2 ( [ P3 ] Eq. ( 40 ) ’s pull-in frequency ) \omega_c\equiv\omega_L\cos\theta_{ss}=\sqrt{\omega_L^2-\Delta\omega^2}\qquad([\text{P3}]\ \text{Eq.}(40)\text{'s pull-in frequency}) ω c ≡ ω L cos θ ss = ω L 2 − Δ ω 2 ([ P3 ] Eq. ( 40 ) ’s pull-in frequency )
At lock center (Δ ω = 0 \Delta\omega=0 Δ ω = 0 ) the corner is widest; at the lock edge (Δ ω → ω L \Delta\omega\to\omega_L Δ ω → ω L ), cos θ s s → 0 \cos\theta_{ss}\to0 cos θ ss → 0 and the high-pass suppression of the oscillator's own noise disappears entirely . (First-order-PLL picture: own noise is high-passed, reference noise is low-passed.)
For a fixed I r m s ≡ ⟨ i i n j 2 ⟩ I_{rms}\equiv\sqrt{\langle i_{inj}^2\rangle} I r m s ≡ ⟨ i inj 2 ⟩ , Cauchy–Schwarz gives the lock-range upper bound ([P3] Eq.(43)–(45), pp.2119–2120):
ω L ∗ = I r m s Γ ~ r m s , i i n j , 0 ∗ ( x ) = ± I r m s Γ ~ r m s Γ ~ ( x ) \omega_L^*=I_{rms}\,\tilde\Gamma_{rms},\qquad i_{inj,0}^*(x)=\pm\frac{I_{rms}}{\tilde\Gamma_{rms}}\tilde\Gamma(x) ω L ∗ = I r m s Γ ~ r m s , i inj , 0 ∗ ( x ) = ± Γ ~ r m s I r m s Γ ~ ( x )
Equality holds iff the injection waveform matches the ISF's shape (matched filter). Pure-sinusoid ISF: sinusoidal injection is already optimal (gain 1). Ring narrow-pulse ISF: gain ≈ η N / 3 \approx\sqrt{\eta N/3} ≈ η N /3 (≈ 2.06 \approx2.06 ≈ 2.06 at N = 17 N=17 N = 17 , matching [P3] Fig.19's "almost doubled").
M:N subharmonic locking / ILFD: ∣ Γ ~ N ∣ \lvert\tilde\Gamma_N\rvert ∣ Γ ~ N ∣ — paper_004
When locked at M ω i n j = N ω o s c M\omega_{inj}=N\omega_{osc} M ω inj = N ω osc (M = 1 M=1 M = 1 is the ÷N N N ILFD case), the half lock range rides on only the N N N -th ISF harmonic ([P4] Eq.(28)–(30), p.2129, verified):
Ω ( θ ) = 1 2 I i n j ∣ Γ ~ N ∣ cos ( N θ + ∠ Γ ~ N ) ⇒ ω L = 1 2 I i n j ∣ Γ ~ N ∣ = I i n j c N 2 q m a x \Omega(\theta)=\frac12 I_{inj}\lvert\tilde\Gamma_N\rvert\cos(N\theta+\angle\tilde\Gamma_N)\ \Rightarrow\
\omega_L=\frac12 I_{inj}\lvert\tilde\Gamma_N\rvert=\frac{I_{inj}\,c_N}{2\,q_{max}} Ω ( θ ) = 2 1 I inj ∣ Γ ~ N ∣ cos ( N θ + ∠ Γ ~ N ) ⇒ ω L = 2 1 I inj ∣ Γ ~ N ∣ = 2 q ma x I inj c N
A half-wave-symmetric ISF (c 2 = c 4 = ⋯ = 0 c_2=c_4=\cdots=0 c 2 = c 4 = ⋯ = 0 ) means ÷2 cannot lock at first order — the same differential-node symmetry that's good news for phase noise is bad news for ILFD (fix: switch to the tail node to pick up c 2 c_2 c 2 ).
Subharmonic multiplication (×N, ILCM): ω L \omega_L ω L , β \beta β , corner — subharmonic_injection
The other half of the duality: at N = 1 N=1 N = 1 , locking is carried by the injection waveform's own N N N -th harmonic (not the ISF's). Canonical: f 0 = 5 f_0=5 f 0 = 5 GHz, q m a x = 1 q_{max}=1 q ma x = 1 pC, N = 20 N=20 N = 20 (f r e f = 250 f_{ref}=250 f r e f = 250 MHz), q i n j = 50 q_{inj}=50 q inj = 50 fC.
Quantity Formula Canonical value Multiplier lock range ω L = 1 2 ∣ I N ∣ ∣ Γ ~ 1 ∣ \omega_L=\tfrac12\vert I_N\vert\vert\tilde\Gamma_1\vert ω L = 2 1 ∣ I N ∣∣ Γ ~ 1 ∣ (impulse train: Δ ω L = q i n j q m a x ⋅ f 0 N \Delta\omega_L=\dfrac{q_{inj}}{q_{max}}\cdot\dfrac{f_0}{N} Δ ω L = q ma x q inj ⋅ N f 0 )f L = 1.989 f_L=1.989 f L = 1.989 MHzRealignment factor β ≡ − q i n j Γ ~ ′ ( θ s s ) \beta\equiv-q_{inj}\tilde\Gamma'(\theta_{ss}) β ≡ − q inj Γ ~ ′ ( θ ss ) (stable for 0 < β < 2 0\lt\beta\lt2 0 < β < 2 , converges in ≈ 1 / β \approx1/\beta ≈ 1/ β injections)0.0498 0.0498 0.0498 Noise corner f c ≈ β f r e f / 2 π f_c\approx\beta f_{ref}/2\pi f c ≈ β f r e f /2 π (= Δ f L \Delta f_L Δ f L at lock center)2.09 2.09 2.09 MHz
ADEV floor: 2 ln 2 ⋅ h − 1 \sqrt{2\ln2\cdot h_{-1}} 2 ln 2 ⋅ h − 1 — allan_variance
σ y , floor = 2 ln 2 ⋅ h − 1 ≈ 1.1774 h − 1 ( flicker FM, the τ -independent floor ) \sigma_{y,\text{floor}}=\sqrt{2\ln2\cdot h_{-1}}\approx1.1774\sqrt{h_{-1}}\qquad(\text{flicker FM, the }\tau\text{-independent floor}) σ y , floor = 2 ln 2 ⋅ h − 1 ≈ 1.1774 h − 1 ( flicker FM, the τ -independent floor )
Canonical (with a 1 / f 3 1/f^3 1/ f 3 corner of 3.2 3.2 3.2 kHz): floor ≈ 1.06 × 10 − 9 \approx1.06\times10^{-9} ≈ 1.06 × 1 0 − 9 (1.1 ppb); knee τ k n e e = 0.3607 / f c ≈ 113 μ \tau_{knee}=0.3607/f_c\approx113\ \mu τ k n ee = 0.3607/ f c ≈ 113 μ s (where the white-FM τ − 1 / 2 \tau^{-1/2} τ − 1/2 segment meets the floor).
PLL peaking: ζ = 0.707 → 2.09 \zeta=0.707\to2.09 ζ = 0.707 → 2.09 dB — pll_noise_budget , supplementary derivation
A type-II loop with a zero always peaks: f p k = f n 2 / ( s + 1 ) f_{pk}=f_n\sqrt{2/(s+1)} f p k = f n 2/ ( s + 1 ) , s = 1 + 1 / ζ 4 s=\sqrt{1+1/\zeta^4} s = 1 + 1/ ζ 4 (golden-ratio easter egg: at ζ = 1 / 2 \zeta=1/\sqrt2 ζ = 1/ 2 the peak value = φ = 1.618 =\varphi=1.618 = φ = 1.618 ).
ζ \zeta ζ f p k / f n f_{pk}/f_n f p k / f n Peaking (dB) Phase margin 0.707 0.786 2.09 65.5° 1.0 0.707 1.25 76.3°
Cascading 20 SONET regenerator stages: 20 × 2.09 = 41.8 20\times2.09=41.8 20 × 2.09 = 41.8 dB, which is why specs cap peaking at the 0.1 dB level per stage.
FOM = 173.8 − 10 log 10 F e f f =173.8-10\log_{10}F_{eff} = 173.8 − 10 log 10 F e f f — fom_limit
F O M = 173.8 dB − 10 log 10 F e f f ( T = 300 K, paired with 1 ⋅ k T , not 2 k T ) \mathrm{FOM}=173.8\ \text{dB}-10\log_{10}F_{eff}\qquad(T=300\ \text{K, paired with }1\cdot kT\text{, not }2kT) FOM = 173.8 dB − 10 log 10 F e f f ( T = 300 K, paired with 1 ⋅ k T , not 2 k T )
Ring ceiling (γ = 2 / 3 , η = 1 \gamma=2/3,\eta=1 γ = 2/3 , η = 1 ): F e f f , m i n = 32 / 9 ⇒ F O M m a x r i n g = 168.32 F_{eff,min}=32/9\Rightarrow\mathrm{FOM}_{max}^{ring}=168.32 F e f f , min = 32/9 ⇒ FOM ma x r in g = 168.32 dB; the LC ceiling rises with Q Q Q (F e f f ∝ 1 / Q 2 F_{eff}\propto1/Q^2 F e f f ∝ 1/ Q 2 ).
Aperture SNR: − 20 log 10 ( 2 π f i n σ t ) -20\log_{10}(2\pi f_{in}\sigma_t) − 20 log 10 ( 2 π f in σ t ) — adc_aperture_jitter
SNR j i t t e r = − 20 log 10 ( 2 π f i n σ t ) dB , ENOB = SNR − 1.76 6.02 bit \text{SNR}_{jitter}=-20\log_{10}(2\pi f_{in}\sigma_t)\ \text{dB},\qquad \text{ENOB}=\frac{\text{SNR}-1.76}{6.02}\ \text{bit} SNR j i tt er = − 20 log 10 ( 2 π f in σ t ) dB , ENOB = 6.02 SNR − 1.76 bit
Canonical σ t = 447.9 \sigma_t=447.9 σ t = 447.9 fs: at f i n = f 0 = 5 f_{in}=f_0=5 f in = f 0 = 5 GHz, 2 π f i n σ t = σ ϕ = 14.07 2\pi f_{in}\sigma_t=\sigma_\phi=14.07 2 π f in σ t = σ ϕ = 14.07 mrad ⇒ \Rightarrow ⇒ SNR = 37.0 =37.0 = 37.0 dB (carried over directly from example C).
TJ = D J δ δ + 2 Q − 1 ( B E R ) σ =\mathrm{DJ}_{\delta\delta}+2Q^{-1}(\mathrm{BER})\sigma = DJ δ δ + 2 Q − 1 ( BER ) σ — dj_dual_dirac
T J ( B E R ) = D J δ δ + 2 Q − 1 ( B E R ) σ \mathrm{TJ}(\mathrm{BER})=\mathrm{DJ}_{\delta\delta}+2\,Q^{-1}(\mathrm{BER})\,\sigma TJ ( BER ) = DJ δ δ + 2 Q − 1 ( BER ) σ
At BER= 10 − 12 =10^{-12} = 1 0 − 12 , Q − 1 = 7.034 Q^{-1}=7.034 Q − 1 = 7.034 , so T J = D J δ δ + 14.07 σ \mathrm{TJ}=\mathrm{DJ}_{\delta\delta}+14.07\,\sigma TJ = DJ δ δ + 14.07 σ . DJ does not change with BER (bounded, paid once); the RJ term grows only slowly as BER tightens (10 − 12 → 10 − 15 10^{-12}\to10^{-15} 1 0 − 12 → 1 0 − 15 : 14.07 σ → 15.88 σ 14.07\sigma\to15.88\sigma 14.07 σ → 15.88 σ ).
Element Phase relation L ( f ) \mathcal{L}(f) L ( f ) bookkeepingIdeal ×N multiplication ϕ o u t = N ϕ i n \phi_{out}=N\phi_{in} ϕ o u t = N ϕ in L + 20 log 10 N \mathcal{L}+20\log_{10}N L + 20 log 10 N Ideal ÷N division ϕ o u t = ϕ i n / N \phi_{out}=\phi_{in}/N ϕ o u t = ϕ in / N L − 20 log 10 N \mathcal{L}-20\log_{10}N L − 20 log 10 N Through a PLL (×N) in-band tracks ref, out-of-band tracks VCO N 2 S r e f ∣ H l p ∣ 2 + S v c o ∣ H h p ∣ 2 N^2S_{ref}\lvert H_{lp}\rvert^2+S_{vco}\lvert H_{hp}\rvert^2 N 2 S r e f ∣ H l p ∣ 2 + S v co ∣ H h p ∣ 2 Buffer/divider additive floor ϕ o u t = ϕ i n + ϕ a d d \phi_{out}=\phi_{in}+\phi_{add} ϕ o u t = ϕ in + ϕ a dd (uncorrelated)L o u t = 10 log 10 ( 10 L i n / 10 + 10 L b u f / 10 ) \mathcal{L}_{out}=10\log_{10}(10^{\mathcal{L}_{in}/10}+10^{\mathcal{L}_{buf}/10}) L o u t = 10 log 10 ( 1 0 L in /10 + 1 0 L b u f /10 ) (convert to linear, add, then convert back to dB )
Conserved quantity: under ideal ×N/÷N, the time-domain σ t \sigma_t σ t (in seconds) never changes — only the L \mathcal{L} L /rad bookkeeping does.
K p u s h K_{push} K p u s h path: S ϕ = K 2 S v / Δ f 2 S_\phi=K^2S_v/\Delta f^2 S ϕ = K 2 S v /Δ f 2 — varactor_tuning_supply_pushing
K V C O ≡ ∂ f 0 ∂ V t u n e , K p u s h ≡ ∂ f 0 ∂ V D D , S ϕ ( Δ f ) = K V C O 2 S v ( Δ f ) Δ f 2 ( the supply version is identical, with K V C O → K p u s h , S v → S v , D D ) K_{VCO}\equiv\frac{\partial f_0}{\partial V_{tune}},\quad K_{push}\equiv\frac{\partial f_0}{\partial V_{DD}},\qquad
S_\phi(\Delta f)=\frac{K_{VCO}^2\,S_v(\Delta f)}{\Delta f^2}\ \ (\text{the supply version is identical, with }K_{VCO}\to K_{push},\ S_v\to S_{v,DD}) K V C O ≡ ∂ V t u n e ∂ f 0 , K p u s h ≡ ∂ V D D ∂ f 0 , S ϕ ( Δ f ) = Δ f 2 K V C O 2 S v ( Δ f ) ( the supply version is identical, with K V C O → K p u s h , S v → S v , D D )
Side by side with the ISF white-noise result: both have a Δ ω 2 \Delta\omega^2 Δ ω 2 /Δ f 2 \Delta f^2 Δ f 2 integrator in the denominator, differing only in what feeds it (Γ r m s / q m a x \Gamma_{rms}/q_{max} Γ r m s / q ma x vs 2 π K V C O 2\pi K_{VCO} 2 π K V C O ). White tune/supply noise → 1 / f 2 \to 1/f^2 → 1/ f 2 ; 1 / f 1/f 1/ f tune/supply noise → 1 / f 3 \to 1/f^3 → 1/ f 3 (parallel to the device c 0 c_0 c 0 mechanism). lab_38 gives a first-principles measurement of K p u s h K_{push} K p u s h (ratio to β \beta β of 1.002).
The five papers in one line each
[P1] Hajimiri–Lee 1998: the ISF theory itself (the oscillator is LTV).
[P2] 1999: ISF applied to rings — closed-form jitter/PN, N N N -independence.
[P3] Hong 2019 I: ISF generalizes Adler → generalized injection locking.
[P4] Hong 2019 II: the APF (amplitude counterpart of the ISF), τ 0 = 2 Q / ω 0 \tau_0=2Q/\omega_0 τ 0 = 2 Q / ω 0 , frequency division.
[P5] a sense amplifier paper, unrelated to the ISF (honestly labeled).
Full cross-reference: paper_summary_table , equation_index .