1,212
edits
Changes
Created page with "== Equation of Translational Dynamics == frame|center where P is the point from which observation is being made, M is the mass of the entire system, a i..."
== 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 Spacecraft Dynamics and Control An Introduction by Ruiter, Forbes, Damaren
If you are done reading this page, you can go back to [[Attitude Determination and Control Subsystem]]
[[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 Spacecraft Dynamics and Control An Introduction by Ruiter, Forbes, Damaren
If you are done reading this page, you can go back to [[Attitude Determination and Control Subsystem]]
