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
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.

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%.…

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.
