Derivation of EoM for two interconnected rigid bodies

Click For Summary
SUMMARY

This discussion focuses on deriving the equations of motion (EoM) for a rocket system that utilizes a movable mass to shift its center of mass for steering. Key considerations include the necessity of understanding angular momentum, specifically tensor of inertia and precession, alongside basic fixed-axis angular momentum. The participant seeks recommendations for textbooks and resources that cover these topics in the context of state space modeling for controller design. Relevant resources include a MIT lecture on rocket dynamics and a Wikipedia article on thrust vectoring.

PREREQUISITES
  • Understanding of angular momentum, including tensor of inertia and precession
  • Familiarity with state space modeling techniques
  • Basic knowledge of rocket dynamics and thrust vectoring
  • Experience with control systems design principles
NEXT STEPS
  • Study "Dynamics of Spacecraft" for insights on equations of motion in aerospace applications
  • Explore "Control Systems Engineering" for advanced state space modeling techniques
  • Research thrust vectoring methods and their impact on rocket stability
  • Examine the principles of center of mass manipulation in dynamic systems
USEFUL FOR

Aerospace engineers, control systems designers, and students interested in rocket dynamics and motion control strategies will benefit from this discussion.

RubinLicht
Messages
131
Reaction score
8
I set a small project for myself to design a controller for a rocket, which moves a mass around to shift the center of mass, in order to steer a rocket.

The picture shows a simplified model of a rocket plus a movable mass. , shown is a rod for the rocket, and a mass for the controller. there is a fixed thrust at the back of the rocket. (which I may change into a control parameter later in the project)

What do I need to know in order to go about writing down the equations of motion for this system? Do I need to know some more hardcore angular momentum (tensor of inertia, precession), or is basic fixed axis angular momentum enough? are there any chapters of textbooks that come to mind that contain the necessary topics I need to put this all in state space so I can design the controller? Any books that are just about deriving physical models of things in general?

Thanks
 

Attachments

  • rocket.jpg
    rocket.jpg
    11.3 KB · Views: 476
Engineering news on Phys.org
I found this article on rocket engines (see page 4 and beyond) This describes a rocket that consumes its fuel and gets lighter but it might give you some insight into your problem.

https://ocw.mit.edu/courses/aeronau...fall-2009/lecture-notes/MIT16_07F09_Lec14.pdf

and here's a wikipedia article on thrust vectoring showing the center of mass and the torque that occurs:

https://en.wikipedia.org/wiki/Thrust_vectoring

Some references I saw said its best to keep the center of mass high on a rocket for stability so maybe shifting the center of mass around isn't a good idea as the rocket may flip. They tend to use fins to steer.
 

Similar threads

  • · Replies 10 ·
Replies
10
Views
2K
  • · Replies 3 ·
Replies
3
Views
4K
  • · Replies 6 ·
Replies
6
Views
665
  • · Replies 12 ·
Replies
12
Views
2K
  • · Replies 8 ·
Replies
8
Views
2K
  • · Replies 3 ·
Replies
3
Views
2K
  • · Replies 8 ·
Replies
8
Views
2K
Replies
3
Views
1K
  • · Replies 6 ·
Replies
6
Views
2K
Replies
12
Views
2K