This page tests everything from the parent note. Work each problem before opening the solution. Levels climb from "can you recognise the formula" up to "can you design a servo loop from scratch."
Recall of the meaning, one line each:
ωn physically
how fast the servo can swing — set by stiffness over inertia.
ζ physically
how the swing settles — under 1 it rings, near 0.7 is ideal.
ωB physically
fastest wiggle the servo can faithfully follow (the −3 dB point).
ωc is
the gain-crossover frequency, where open-loop magnitude = 1 and stability is judged.
On the jω axis, a pure delay e−sτ affects
only phase (−ωτ), never magnitude (which stays 1 there).
WHAT we do: match term-by-term to the standard denominator.
WHY: the standard form is a template — the numbers slot into named slots, no derivation needed.
Constant term ωn2=2500⇒ωn=2500===50rad/s==.
Middle term 2ζωn=50⇒ζ=2×5050===0.5==.
The numerator equals ωn2=2500, confirming unit DC gain (at s=0, G=2500/2500=1).
Recall Solution L1.2
WHAT/WHY: on the jω axis (i.e. evaluating the frequency response at s=jω) a pure delay has magnitude exactly 1 — it only rotates phase. This qualifier matters: off the imaginary axis, in the general complex-s plane, ∣e−sτ∣ is not 1. Frequency-response magnitude and general-s magnitude are different things; the "always 1" claim is a statement about the jω axis only.
(a) ∣e−jωτ∣===1== for any real ω (the exponent is purely imaginary, so it is a unit-modulus rotation).
(b) Phase =−ωτ=−30×0.01=−0.30rad. In degrees =−0.30×57.2958===−17.2∘==.
Because ζ<1/2 the system is lightly damped, so ωB>ωn (it resonates before rolling off).
Recall Solution L2.2
WHAT/WHY: delay phase is Δϕ=−ωcτ evaluated at crossoverωc (defined above), because crossover is where the −180∘ stability limit is judged.
Δϕ=−ωcτ=−20×0.025=−0.50rad=−0.50×57.2958=−28.6∘.
The size of the loss (what we "spend") is ==28.6∘== — same magnitude, positive because we are quoting how much margin is consumed.
Remaining margin =50∘−28.6∘===21.4∘== — thin (below the 30∘ comfort line).
Step 1 — exploit the ζ=0.707 identity. At ζ=1/2, 1−2ζ2=0, so
ωB=ωn0+0+1=ωn.
Therefore ωn=120rad/s directly. This is exactly why we design to 0.707 — the algebra collapses.
Step 2 — back out stiffness. From ωn2=(k+K)/J:
k+K=ωn2J=1202×0.6=14400×0.6===8640N⋅m/rad==.
Recall Solution L3.2
WHAT we do: plug each ζ into the bandwidth radical. WHY: we want to see howωB moves relative to ωn as damping changes — one variable (ζ) swept, everything else fixed, so the result isolates damping's effect alone.
Use ωB=ωn(1−2ζ2)+(1−2ζ2)2+1.
ζ=0.5: WHAT — 1−2ζ2=0.5 (positive, so the light damping pushes ωB above ωn). ωB=1000.5+1.25=1000.5+1.118=1001.618===127.2rad/s==.
ζ=0.707: WHAT — 1−2ζ2=0, the term vanishes and the radical collapses to 1. ωB=1000+1===100rad/s==.
ζ=1.0: WHAT — 1−2ζ2=−1 (negative, so heavy damping drags ωB below ωn). ωB=100−1+2=100−1+1.4142=1000.4142===64.4rad/s==.
Trend: as damping rises, ωBfalls — heavy damping trades away following-speed for calm settling.
Reading the figure (s01): the horizontal axis is the damping ratio ζ and the vertical axis is the bandwidth ratio ωB/ωn. The red curve is that ratio; it starts above 1 (light damping, fast following), crosses the dashed horizontal line ωB/ωn=1 exactly at the dotted vertical ζ=1/2, and continues downward. The three black dots are our three answers (1.27, 1.00, 0.64) — visual proof that the sole reason ωB=ωn is special is that we chose to land on that crossing point.
Synthesis point: raising gain raised ωc, and since delay phase magnitude is proportional toωc, the loss grew from 17.2∘ to 28.6∘ — gain made it worse. On the jω axis the magnitude of e−jωτ is 1 at every frequency, so gain cannot "outrun" a delay; only cutting τ (faster computer / higher sample rate, see Digital control — sampling & computational delay) or lowering bandwidth helps.
Recall Solution L4.2
2τ=0.02s.
Zero: numerator 1−0.02s=0⇒s=+τ2=+0.042===+50s−1==. This sits in the right half-plane (positive real part).
The right-half-plane zero at +50 is the fingerprint: it makes the output initially move the wrong way (undershoot), which is the destabilising essence of transport delay. See Padé approximation of transport delay for higher orders.
Reading the figure (s02): the horizontal axis is Re(s) and the vertical axis is Im(s) — the complex s-plane. The shaded band on the right marks the right half-plane. The black "×" at −50 is the harmless stable pole; the red open circle at +50 is the zero — placing it inside the shaded (right-half) region is exactly the picture of "the output first goes the wrong way." The mirror symmetry about the imaginary axis is why first-order Padé keeps magnitude flat while injecting pure phase lag.
Step 1 — bandwidth floor (Req 1). Need ωB=ωn≥5×12=60rad/s.
Step 2 — bending ceiling (Req 2). Need ωn<180rad/s; a common rule keeps it well below, say ≤90. A choice of ωn=80rad/s sits comfortably in the window [60,90].
Step 3 — delay check (Req 3). Delay phase magnitude at crossover:
∣Δϕ∣=ωcτ=12×0.015=0.18rad=0.18×57.2958===10.3∘==≤12∘.✓
(Note this depends only on ωc and τ, not on ωn — so it passes regardless of the ωn pick.)
Step 4 — hardware from ωn=80, ζ=0.707, J=0.7.k+K=ωn2J=802×0.7=6400×0.7===4480N⋅m/rad==.c=2ζ(k+K)J=2(0.707)4480×0.7=1.4143136=1.414×56===79.2N⋅m⋅s==.
Verdict:ωn=80 rad/s gives ωB=80≥60 ✓, sits below the 180 rad/s bending mode ✓, and the delay spends only 10.3∘≤12∘ ✓. All three requirements met.
Recall Solution L5.2
The bandwidth floor (≥60) is satisfied, but ωn=170 places the servo's own −3 dB edge only 180−170=10rad/s (≈6%) below the bending mode. The servo would drive the flexible structure near resonance; small gain/phase errors turn TVC into an oscillator. The margin to 180 is far too thin — you would need a notch filter (Structural bending modes & notch filters) or, better, back off to ωn≈80. Fast is good; too fast collides with structure.