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Case Studies · Robotics & UAS hardware

Sizing drone landing gear to the landing, not the datasheet

A printed cantilever leg that absorbs a hard landing — with the factor of safety computed by the energy method, not asserted.

The result at a glance

2.15×
FoS at a 1.0 m/s hard landing
1.52×
FoS on a tilted 2-leg touchdown (no yield)
3.0 J
descent energy absorbed
0.00%
FEA equilibrium error (mesh valid)

Problem → built result

What we solved

Drone landing gear is the part everyone copies off a free STL and nobody analyzes. That's fine until a commercial aircraft — a survey or inspection rig carrying a gimbal worth more than the drone — comes down hard. A leg that cracks on a 1 m/s touchdown costs a re-fly, a possible gimbal strike, and a grounded job.…

What we built

Treat the leg as what it physically is: a cantilever spring. Model it parametrically — a mount pad, a tapered blade strut, a skid foot — solve it once under a reference load, and read its stiffness and its stress-per-newton from that one finite-element analysis.

Assembly render — Nylon-PA cantilever leg, set of four

How we proved it

The engineering behind the result.

Material matched to the duty, not the spec sheet

Landing gear is an impact-and-fatigue part, and that pair narrows the field hard. Nylon-PA12 is the one common FDM polymer that takes both: TPU is too soft for a structural leg, CF-nylon is explicitly the wrong call for impact toughness, and PETG and PLA fail on fatigue.…

The factor of safety is an output

At the rated 1.0 m/s hard landing each leg holds 2.15× inside the as-printed allowable. A tilted touchdown that drops the whole descent energy onto just two legs still holds 1.52× — no yield. Standing at rest the margin is 64×.…

Proof the model is real

The reactions balance the applied landing load to 0.00% — a wrong finite-element mesh can't satisfy equilibrium, so that's the mesh validating itself. An independent hand-calc of the leg's stiffness as an inclined cantilever agrees with the FEA to 12%.…

Landing-impact FEA — von Mises field under the energy-method peak ground reaction

Delivered result

Evidence a buyer can use.

A landing-gear leg that ships as a configurable product sized to the customer's aircraft, with the FEA that proves it survives the landing — not a traced STL with a hopeful weight on it. The honest gates travel with it: the rating is a single hard landing (repeated hard landings are a fatigue duty, which is why we chose nylon and offer a cyclic test), and th…

Application notes

The factor of safety is for a single hard landing. Repeated hard landings are a fatigue duty — Nylon-PA resists interlayer fatigue better than PETG or PLA, but we offer a cyclic-landing test rather than claim a life. The energy method assumes elastic absorption; a TPU skid foot (offered) softens the peak further.…

Bring us your version

Configure the Commercial Drone Landing Gear.

Send the part, drawing, sample, or operating requirements. We’ll quote the engineering and build together.