The present invention provides a large-tolerance deployable double-point special-shaped positioning and guiding mechanism and a
tolerance design method. The mechanism comprises two sets of deployable positioning and guiding mechanisms with parallel and symmetric structures and similar structures, both of which are composed of an active end and a passive end. The passive end includes a base and a guiding column, and is fixed on the outer platform of the cabin. The active end includes a deployable mechanism, a compression and release mechanism, a connecting rod, a positioning and guiding hole, and a
visualization window, and is connected to a space
payload. The guiding column corresponds to the guiding hole and is divided into a small column section, a large column section, and a transition section. The positioning and guiding mechanism is divided into a fixed and a floating fit, and the corresponding positioning and guiding holes are circular and
waist-shaped respectively. The present invention saves space, has a large deployment
stroke, controllable speed, improves the bending and torsion resistance capabilities of the space
payload, makes it have the characteristics of large stiffness, reliable connection, etc., and has a large tolerance
adaptation ability during guiding, can better realize the positioning and guiding function, and provides
technical support for installing a large space
payload at a set position outside the
spacecraft cabin.