Publication Date:
2019-08-28
Description:
The construction of the programmed motion of a multileg bounding vehicle in the flight was studied. An algorithm is given for solving the boundary value problem for constructing this programmed motion. If the motion is shown to be symmetrical, a simplified use of the algorithm can be applied. A method is proposed for nonimpact of the legs during lift-off of the vehicle, and for softness at touchdown. Tables are utilized to construct this programmed motion over a broad set of standard motion conditions.
Keywords:
MECHANICAL ENGINEERING
Type:
NASA-TM-75668
,
PREPRINT-26
Format:
application/pdf
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