Difference between revisions of "Equations of Rigid Body Rotational and Translational Dynamics"
(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...") |
|||
| Line 5: | Line 5: | ||
==Equation of Rotational Dynamics == | ==Equation of Rotational Dynamics == | ||
[[File:RotDyn.jpg|frame|center]] | [[File:RotDyn.jpg|frame|center]] | ||
| − | Derivation of these equations can be found in Spacecraft Dynamics and Control An Introduction by Ruiter, Forbes, Damaren | + | 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]''' |
| − | + | ---- | |
If you are done reading this page, you can go back to [[Attitude Determination and Control Subsystem]] | If you are done reading this page, you can go back to [[Attitude Determination and Control Subsystem]] | ||
Latest revision as of 20:19, 1 February 2018
Equation of Translational Dynamics
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
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
