The invention relates to aircraft landing gear (0) having a male part (M0, M1, M3) interlocked with a female part (F0, F1, F2, F3) along an interlocking direction (D). The external contact surface of the male part (M0...
标准号:
WO2023/066970(A1)
The invention relates to aircraft landing gear (0) having a male part (M0, M1, M3) interlocked with a female part (F0, F1, F2, F3) along an interlocking direction (D). The external contact surface of the male part (M0, M1, M3), when it is observed along the interlocking direction (D), is an exclusively convex closed surface having external contact surface portions in the form of rounded lobes (L1, L2, L3, L4) that form obstacles to the pivoting of the female part (F0, F1, F2, F3) with respect to the male part (M0, M1, M3) about the interlocking direction (D). The invention also relates to an aircraft having such landing gear.
Disclosed are a method and a system for estimating a height shape of a road surface in a road scene. The method comprises a step of obtaining an original disparity map of the road scene;a step of detecting a road-surf...
标准号:
JP6442834(B2)
Disclosed are a method and a system for estimating a height shape of a road surface in a road scene. The method comprises a step of obtaining an original disparity map of the road scene;a step of detecting a road-surface region of interest based on the original disparity map;a step of determining plural road-surface points of interest based on the road-surface region of interest;and a step of estimating the height shape of the road surface in the road scene based on the plural road-surface points of interest.
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