Vladimir S. Syromiatnikov Spacecraft Docing Devices deom SSI

this moment are no less than a certain value which is sufficient to activate the One can also assign additional criteria for failure to dock, for example, exceeding an acceptable duration of the process from first contact to linkage, etc. 4.3.2. A Model which Considers Deformation of the Shock Absorbers The position of the rod of the docking mechanism is given here by radius vector When there are deformations of the shock absorbers the vector may rotate in yaw and pitch and contract (Figure 4.2); its components, considering parameter w in system of coordinates 1 is are equal to: Figure 4.2. Schematic for finding the point of interaction (T.B.) for a “rod and cone” docking device considering deformation of the shock absorbers.

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