3.5.45 · D4Guidance, Navigation & Control (GNC)

Exercises — TVC dynamics — gimbal servo bandwidth, time delay

2,374 words11 min readBack to topic

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:

physically
how fast the servo can swing — set by stiffness over inertia.
physically
how the swing settles — under 1 it rings, near 0.7 is ideal.
physically
fastest wiggle the servo can faithfully follow (the dB point).
is
the gain-crossover frequency, where open-loop magnitude = 1 and stability is judged.
On the axis, a pure delay affects
only phase (), never magnitude (which stays 1 there).

Level 1 — Recognition

Recall Solution L1.1

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 .
  • Middle term .

The numerator equals , confirming unit DC gain (at , ).

Recall Solution L1.2

WHAT/WHY: on the axis (i.e. evaluating the frequency response at ) a pure delay has magnitude exactly 1 — it only rotates phase. This qualifier matters: off the imaginary axis, in the general complex- plane, is not 1. Frequency-response magnitude and general- magnitude are different things; the "always 1" claim is a statement about the axis only.

  • (a) for any real (the exponent is purely imaginary, so it is a unit-modulus rotation).
  • (b) Phase . In degrees .

Level 2 — Application

Recall Solution L2.1

Step 1 — (WHY first: it sets the scale for everything else).

Step 2 — .

Step 3 — . Compute .

Because the system is lightly damped, so (it resonates before rolling off).

Recall Solution L2.2

WHAT/WHY: delay phase is evaluated at crossover (defined above), because crossover is where the stability limit is judged. The size of the loss (what we "spend") is — same magnitude, positive because we are quoting how much margin is consumed. Remaining margin — thin (below the comfort line).


Level 3 — Analysis

Recall Solution L3.1

Step 1 — exploit the identity. At , , so Therefore directly. This is exactly why we design to 0.707 — the algebra collapses.

Step 2 — back out stiffness. From :

Figure — TVC dynamics — gimbal servo bandwidth, time delay
Recall Solution L3.2

WHAT we do: plug each into the bandwidth radical. WHY: we want to see how moves relative to as damping changes — one variable () swept, everything else fixed, so the result isolates damping's effect alone.

Use .

  • : WHAT (positive, so the light damping pushes above ). .
  • : WHAT, the term vanishes and the radical collapses to 1. .
  • : WHAT (negative, so heavy damping drags below ). .

Trend: as damping rises, falls — heavy damping trades away following-speed for calm settling.

Reading the figure (s01): the horizontal axis is the damping ratio and the vertical axis is the bandwidth ratio . The red curve is that ratio; it starts above 1 (light damping, fast following), crosses the dashed horizontal line exactly at the dotted vertical , and continues downward. The three black dots are our three answers (, , ) — visual proof that the sole reason is special is that we chose to land on that crossing point.


Level 4 — Synthesis

Recall Solution L4.1

The delay's phase contribution is (a lag, hence negative); we quote its magnitude as the loss.

  • Before: .
  • After: .

Synthesis point: raising gain raised , and since delay phase magnitude is proportional to , the loss grew from to — gain made it worse. On the axis the magnitude of is 1 at every frequency, so gain cannot "outrun" a delay; only cutting (faster computer / higher sample rate, see Digital control — sampling & computational delay) or lowering bandwidth helps.

Figure — TVC dynamics — gimbal servo bandwidth, time delay
Recall Solution L4.2

.

  • Zero: numerator . This sits in the right half-plane (positive real part).
  • Pole: denominator (left half-plane, stable).

The right-half-plane zero at 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 and the vertical axis is — the complex -plane. The shaded band on the right marks the right half-plane. The black "" at is the harmless stable pole; the red open circle at 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.


Level 5 — Mastery

Recall Solution L5.1

Step 1 — bandwidth floor (Req 1). Need .

Step 2 — bending ceiling (Req 2). Need ; a common rule keeps it well below, say . A choice of sits comfortably in the window .

Step 3 — delay check (Req 3). Delay phase magnitude at crossover: (Note this depends only on and , not on — so it passes regardless of the pick.)

Step 4 — hardware from , , .

Verdict: rad/s gives ✓, sits below the rad/s bending mode ✓, and the delay spends only ✓. All three requirements met.

Recall Solution L5.2

The bandwidth floor () is satisfied, but places the servo's own dB edge only () 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 is far too thin — you would need a notch filter (Structural bending modes & notch filters) or, better, back off to . Fast is good; too fast collides with structure.


Recall One-screen summary of every answer
  • L1.1: , . L1.2: mag , phase .
  • L2.1: , , . L2.2: eaten, left.
  • L3.1: , . L3.2: .
  • L4.1: . L4.2: zero , pole .
  • L5.1: valid, , , .