Here's my analysis. The headline findings: the pitch lever from your thrusters is the **vertical** depth below the CG (≈6.6–8.6 ft), not the 38-ft fore-aft leg spacing — horizontal thrust lines create no pitch couple, so your instinct that "right at the bottom works better" is correct, for two reasons. With realistic thrust headroom you get ~5–10% pitch reduction; with ~4× more thrust authority, ~30%. Full details, tables, and the occupant-perception answer are in the HTML file below — save it as `pitch-damping.html` and drop it into your site. ```html Seastead Pitch Damping via Thrust Modulation — 4-ft Chop @ 4 mph

Active Thrust Modulation for Pitch Damping
Seastead in 4-ft Caribbean Chop @ 4 mph

First-order seakeeping estimate • head seas vs. following seas • thrusters 2 ft up vs. at leg bottom • what occupants will actually feel

Bottom Line

The mechanism is real, but the lever arm is smaller than it looks. A horizontal thruster force creates pitch moment only through its vertical offset below the CG: M = h · ΔT, with h ≈ 6.6 ft (2 ft up) or 8.6 ft (at the bottom). The 38-ft fore-aft leg spacing contributes nothing — parallel horizontal forces make no pitch couple.

How much reduction? With realistic ±1,000 lbf of total thrust modulation: ~5–10% less pitch. With ±2,750 lbf (comfort cap): ~20%. With ±4,000 lbf: ~30%. It is damping, not cancellation — the thrusters trim the resonant peak, they cannot flatten the sea.

Your instinct is right: bottom-mounted thrusters deliver ~1.5× the damping of "2 ft up" — about 30% from the longer arm, the rest from never losing thrust to ventilation in wave troughs.

Will people notice? At standard thrust: probably neither the improvement nor the thrust changes — the system works quietly on the resonant peaks. At upsized thrust: yes, a visibly flatter ride (welcomed), plus a gentle ±0.1 g speed "breathing" that most people tolerate fine if you cap it there.

Tn ≈ 5.3 s
Natural pitch period (est.)
4.6 s / 6.9 s
Encounter period @ 4 mph — head / following
7.0° / 7.5°
Base pitch amplitude — head / following
−10% … −31%
Achievable pitch reduction (std → upsized thrust)

1 · The Physics — Why Depth Matters and Spacing Doesn't

A thruster pushes the boat along the leg axis (horizontal). The torque about the CG is r × F. Because the force is horizontal, only the vertical part of the moment arm survives:

Mpitch = h · ΔT     h = vertical distance, CG → thrust line
h ≈ 8.6 ft (thrusters at leg bottom, CG ≈ +1.3 ft)  •  h ≈ 6.6 ft (thrusters 2 ft up)
waterline 4-ft chop living area (side view) (rear legs overlap in side view) CG ≈ +1.3 ft 2 ft up bottom ΔT h₁ ≈ 6.6 ft h₂ ≈ 8.6 ft Pitch moment = h × ΔT — depth sets the lever, not the 38-ft leg spacing
Schematic, not to scale. Forward thrust applied below the CG bows the nose up; modulating total thrust at the pitch rate opposes rotation — that is the whole game.

2 · Estimated Pitch Amplitudes — 4-ft / 5.5-s Chop Component, 4 mph

Configuration Thrust modulation Head seas
(into waves)
Δ Following seas
(away from waves)
Δ
Base case — no modulated thrust 7.0° 7.5°
Modulated thrusters 2 ft above leg bottom ±850 lbf (ventilation-derated) 6.5°−7% 7.1°−4%
Modulated thrusters at leg bottom ±1,000 lbf 6.3°−10% 7.0°−7%
★ Bottom mount, comfort-capped (recommended) ±2,750 lbf 5.3°−23% 6.1°−19%
Bottom mount, upsized thrusters (sensitivity) ±4,000 lbf 4.8°−31% 5.5°−27%

How to read this: values are the steady-state pitch amplitude to a regular 4-ft, 5.5-s wave component at 4 mph — the worst-case "slice" of a real sea. In genuine irregular Caribbean chop, significant pitch is roughly ⅔ of these figures (base case ≈ 4.5–5° significant). Percent reductions are more robust than the absolute numbers and hold approximately across the 4.5–7 s chop-period band.

Why head and following come out nearly equal

The estimated natural pitch period (Tn ≈ 5.3 s) sits between the head-sea encounter period (4.6 s) and the following-sea encounter period (6.9 s) at 4 mph — so both headings run near resonance. Which one is nominally worse flips with the added-mass assumption (Tn anywhere in 4.5–7 s); the percentage benefit of active thrust does not. Note also that at zero speed both headings converge on the same near-resonant condition — this hull will be pitch-lively in 5-s chop even parked, which is exactly what your heave plates are for.

3 · Visual Comparison

Head seas (into the waves)

Base — no active thrust
7.0°
Active — 2 ft up (±850 lbf)
6.5°
Active — bottom (±1,000 lbf)
6.3°
★ Bottom, comfort cap (±2,750)
5.3°
Bottom, upsized (±4,000 lbf)
4.8°

Following seas (away from the waves)

Base — no active thrust
7.5°
Active — 2 ft up (±850 lbf)
7.1°
Active — bottom (±1,000 lbf)
7.0°
★ Bottom, comfort cap (±2,750)
6.1°
Bottom, upsized (±4,000 lbf)
5.5°

4 · What Occupants Will Feel

Total-thrust modulation necessarily pulses the boat's speed (there is no way around it with fixed horizontal thrusters at a common depth). Here is that side effect versus human perception thresholds:

SensationStd thrust (±1,000 lbf)Comfort cap (±2,750 lbf)Upsized (±4,000 lbf)Human detection
Pitch amplitude change −7…−10%−19…−23%−27…−31% Visual/vestibular detection typically needs a 15–20% amplitude change; under ~10% is rarely noticed consciously.
Speed pulsing (amplitude) ±0.5 mph±1.3 mph±1.9 mph Below ~0.5 mph at a 5-s period: imperceptible "breathing."
Longitudinal acceleration 0.036 g0.10 g0.145 g Perception threshold ≈ 0.02–0.05 g; general-comfort guideline ≈ 0.10 g for horizontal oscillation under 0.5 Hz.
Sound Slow RPM swells on quiet rim drives A soft rhythmic whoosh; far less objectionable than diesel hunting. Rarely commented on.

Verdict

5 · Recommendations

  1. Mount the thrusters at the very bottom of the legs. Your instinct was correct — but for the right reason: the pitch lever is the vertical arm below the CG (8.6 ft vs 6.6 ft, +30%), plus guaranteed ventilation-free thrust in troughs. The fore-aft leg spacing contributes no pitch moment at all.
  2. Size for at least ±1,000 lbf of total modulation (i.e., each rim drive ~100 lbf continuous / 200 lbf peak beyond its ~25 lbf cruise share). Energy cost is trivial: fully saturated control averages ~5 kW against a ~300 kWh battery — the limit is installed thrust, not stored energy.
  3. Cap control thrust near ±2,750 lbf (≈0.10 g surge) as a comfort governor; allow brief excursions beyond only for emergency attitude authority.
  4. Control law: IMU pitch-rate feedback, ΔT = −K·θ̇ with saturation and slew limiting, coordinated with the speed autopilot (either accept the ±1 mph breathing or feed-forward-cancel it in the speed loop).
  5. Don't expect the thrusters to carry the ride alone. Heave plates and vertical mass distribution set the base damping — each +0.05 of passive damping ratio is worth roughly another 8–10% off the base pitch. Active thrust trims the resonant peak on top of that.
  6. Future upgrade path: active fins near the leg bottoms would generate vertical lift forces — a pure pitch couple with zero speed pulsing (the classic SWATH stabilizer solution). That decouples pitch control from propulsion entirely and is where an order-of-magnitude improvement lives.
  7. Cheap alternative with staggered depths: mounting front-leg thrusters deeper than rear-leg thrusters would let fore/aft differential thrust create a couple at constant total thrust (moment arm = the depth difference). With a 2-ft stagger the arm is only 2 ft — 4× weaker than the total-thrust scheme — so it's a niche option, not a winner.
  8. When parked on tension legs, the mooring screws stiffen pitch and the controller can idle — no conflict.

6 · Method & Assumptions (so you can rerun it with real numbers)

ParameterValue usedBasis
Displacement27,500 lb (m = 854 slugs)Your spec
Pitch inertia incl. added massI ≈ 7.0×10⁵ slug·ft²Dry estimate ≈ 4.3×10⁵ (masses at corners dominate) + added inertia ≈ 2.7×10⁵ from heaving legs
Waterplane 2nd moment / pitch stiffnessIwp ≈ 15,000 ft⁴ → K ≈ 9.8×10⁵ ft·lb/radThree foil sections (~17 ft² each) at r ≈ 24.5 ft; consistent with your "1 ft = 1/7 of buoyancy"
Natural pitch periodTn = 2π√(I/K) ≈ 5.3 sDerived
Passive damping ratioζ₀ = 0.16Heave plates + wave radiation; SWATH-type typical 0.10–0.25
Sea stateH = 4 ft (a = 2 ft), T = 5.5 s, deep water; λ ≈ 152 ft, max wave slope 4.6°Representative Caribbean trade chop
Speed / encounter4 mph = 5.87 ft/s → Te = 4.6 s (head), 6.9 s (following)ωe = ω ± kU
CG height≈ +1.3 ft above WLBatteries (25% of load) low in legs pull it down
Thruster ratingsAssumed: 25 lbf ea cruise; 100 lbf cont. / 200 lbf peak ea → ±1,000 lbf total modulationReplace with your actuals — results scale almost linearly with available ΔT
Quasi-static pitch (contouring)θqs ≈ 3.6°wave slope × depth attenuation e^(−k·z̄) × footprint averaging sin(kd/2)/(kd/2)
Single-DOF pitch response:  I·θ̈ + C·θ̇ + K·θ = Mwave(t)
Active control:  ΔT = −Kc·θ̇ (saturated at ΔTmax)  →  C = Cpassive + h·Kc
Amplifier:  D(r,ζ) = 1 / √[ (1−r²)² + (2ζr)² ],  r = ωen,  θ = θqs·D
Gains set so peaks just reach saturation; checked self-consistently (no case exceeded ±ΔTmax).

Actuation lag (<0.3 s) is negligible against 4.6–6.9 s periods and was ignored. Ventilation derate for the "2 ft up" case: usable modulation reduced ~15% (trough submergence ≈ 2.2 thruster diameters).

``` A few things worth flagging outside the document: 1. **The key correction to the premise:** differential fore/aft thrust (more at the bow, less at the stern) produces *zero* pitch moment if all thrusters are at the same depth — parallel horizontal forces can't make a couple. The lever is purely the vertical drop from CG to thrust line. This is why "at the bottom" wins, and it's also why the control has to be *total*-thrust modulation, which inevitably pulses speed slightly (quantified in §4). 2. **Both headings are near resonance at 4 mph** (encounter periods 4.6 s and 6.9 s bracket the ~5.3 s natural pitch period), so head vs. following is nearly a tie in the nominal model — and which one is worse flips with the added-mass assumption. The percentage improvements are the trustworthy numbers. 3. **The thruster ratings were assumed** (100 lbf continuous / 200 lbf peak each). If your actual rim drives differ, the results scale almost linearly with available total thrust — swap the numbers into §6 and the conclusions update proportionally.