View source for Equations of Rigid Body Rotational and Translational Dynamics

== Equation of Translational Dynamics ==
[[File:Equation2.gif|frame|center]]
where P is the point from which observation is being made, M is the mass of the entire system, a is acceleration and CM is the centre of mass of system

==Equation of Rotational Dynamics ==
[[File:RotDyn.jpg|frame|center]]
Derivation of these equations can be found in '''[https://www.amazon.com/Spacecraft-Dynamics-Control-Anton-Ruiter/dp/1118342364 Spacecraft Dynamics and Control An Introduction by Ruiter, Forbes, Damaren]'''
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