ASC_3 - % Kevin Menear % Multibody Dynamics - Spring '08 %...

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Sheet1 Page 1 % Kevin Menear % Multibody Dynamics - Spring '08 % Autonomous Satellite Capture by a Space Robot % % Body J - Main robot body % Body K - Robot arm directly attached to main body % Body L - End robot arm % Point O - Newtonian origin % Point SO - COM of system % Point JO - COM of body J % Point KO - COM of body K % Point LO - COM of body L % Point U - Point coincident with bodies J and K % Point V - Point coincident with bodies K and L % Point P - Point representing satellite body, following a prescribed path % Point PO - Point about which point P rotates % Point Q - Point on body L that will be coincident with point P % MJ - Mass of body J % MKL - Mass of bodies K and L % Q1 - Angle between N and J reference frames % Q2 - Angle between J and K reference frames % Q3 - Angle between K and L reference frames % Q4 - Magnitude of position vector from O to JO in the N1 direction % Q5 - Magnitude of position vector from O to JO in the N2 direction % THETA - Angle between N and P references frames
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This note was uploaded on 04/16/2008 for the course MANE Engineerin taught by Professor Scarton during the Spring '08 term at Rensselaer Polytechnic Institute.

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ASC_3 - % Kevin Menear % Multibody Dynamics - Spring '08 %...

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