Rockets and inverted pendulums

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    Rocket Rockets
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Discussion Overview

The discussion revolves around the stability of rockets during flight, particularly focusing on how they are not flipped over by their thrusters, especially in the absence of fins. Participants explore concepts related to rocket dynamics, control systems, and comparisons to inverted pendulums.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested

Main Points Raised

  • One participant expresses confusion about how rockets remain stable without fins, likening their behavior to that of an inverted pendulum.
  • Another participant suggests that the ability to turn rocket motors provides balance and horizontal force, contributing to stability.
  • There is a discussion about the role of control systems, with some participants proposing that stability is achieved through regulators like PID controllers, while others argue that higher-order filters are more appropriate.
  • Several participants mention that rockets can be stabilized at sea level using fins, but debate the effectiveness of fixed motors in achieving stability.
  • Concerns are raised about the speed of rockets at sea level, with one participant questioning the assertion that rockets have no speed upon launch.
  • Participants discuss the center of pressure and center of mass in relation to stability, particularly in the context of New Year rockets.
  • A participant warns against experimenting with removing stabilizing rods from rockets, emphasizing the dangers involved.
  • Another participant critiques the analogy of rockets to pendulums, arguing that the dynamics of rockets do not align with those of inverted or normal pendulums due to the nature of the forces involved.

Areas of Agreement / Disagreement

Participants express multiple competing views regarding the stability of rockets, the effectiveness of control systems, and the validity of pendulum analogies. The discussion remains unresolved with no consensus reached on these points.

Contextual Notes

Participants highlight limitations in understanding related to the dynamics of rockets, the influence of air resistance, and the assumptions made about speed and stability at sea level.

CyberneticsInside
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Hi, I can´t understand how a rocket is not flipped over by the thrusters (especially without finns). I know this is a general misconception of how a rocket works, but it seams intuitive that it would behave like a inverted pendulum, since the force works below the center of mass, of the rocket.

Does someone have a dumbed down explanation?
 
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The rocket motors can be turned some degrees. Hence the rocket can be balanced, giving the lower end of the rocket some horizontal force.
 
Have a look at this video:



After about 1:42 min., you can see the motors turn slightly.
 
Ok, thanks for the response.
So the stability is caused på some kind regulator, f. instance a PID? Meaning a fixed motor will be un-stable?
 
CyberneticsInside said:
So the stability is caused på some kind regulator, f. instance a PID? Meaning a fixed motor will be un-stable?
I don't think the term "PID" ( first order filter ) can be used. I think that a system of higher order filters are used for the purpose.

Yes, with a fixed motor, the rocket will be unstable.
 
Hesch said:
I don't think the term "PID" ( first order filter ) can be used. I think that a system of higher order filters are used for the purpose.

Yes, with a fixed motor, the rocket will be unstable.
oh i see, thank you.
 
But at sea level, a rocket may be stabilized with finns on the body? (Fixed motor)
 
CyberneticsInside said:
But at sea level, a rocket may be stabilized with finns on the body? (Fixed motor)

Several types of aircraft have been built with rocket engines - mostly for research purposes . These had control surfaces .

One of the most successful was the X15 .



https://en.wikipedia.org/wiki/North_American_X-15
 
CyberneticsInside said:
But at sea level, a rocket may be stabilized with finns on the body? (Fixed motor)
A rocket, that is launched at sea level, has no speed. Thus wings/finns will not work. But a missile flying horizontally at sea level at high speed may be stabilized by means of wings/finns.

New year rockets are stable with a "fixed motor", because the motor is placed at the top og the rocket. ( Front wheel drive ).
 
  • #10
Hesch said:
A rocket, that is launched at sea level, has no speed. Thus wings/finns will not work. But a missile flying horizontally at sea level at high speed may be stabilized by means of wings/finns.

New year rockets are stable with a "fixed motor", because the motor is placed at the top og the rocket. ( Front wheel drive ).

I don´t follow when you say rockets at sea level has no speed. What do you mean ?
And I believed that the center of pressure is further to the ground than the center of mass, in new years rocket.

I saw an old picture of a ¨Front wheel´´ driven rocket, but it was highly unstable, and crashed shortly after launch. Should think a rocket like that, would be stable.

http://history.info/wp-content/uploads/2015/03/Modern-rocket.jpg
 
  • #11
CyberneticsInside said:
I don´t follow when you say rockets at sea level has no speed. What do you mean ?
Well, I assume that the rocket is not launched submerged, and if the astronauts are to be accelerated by say 5g, it will take some time before the rocket has achieved a speed whereby it can be controlled by wings/finns.

I believed that the center of pressure is further to the ground than the center of mass, in new years rocket.

Well, it has this rod at its tail. Try to remove/shorten the rod next new year, and test the result.
( Keep distance )
.
 
Last edited:
  • #12
Oh yeah. I did not think of the rod. Sounds interesting to try tough (remive the rod)
 
  • #13
CyberneticsInside said:
Sounds interesting to try tough (remive the rod)
It is not interesting, it is dangerous.

The rocket will be completely out of control.
 
  • #14
Hesch said:
It is not interesting, it is dangerous.

The rocket will be completely out of control.
Yeah, obviously :p
 
  • #15
Hesch said:
It is not interesting, it is dangerous.

The rocket will be completely out of control.

All the more reason to applaud the early rocket pioneers who made rockets work without the benefit of today's control systems. And don't forget the Chineese who were the first (I think) to make practical skyrocket fireworks. It makes on think again about the role of the stick in a bottle rocket.
 
  • #16
Although it is attractive to view a rocket standing on fixed rear-mounted engines as an inverted pendulum and a rocket hanging from fixed front-mounted engines as a normal pendulum, both views are incorrect. Let us neglect the influence of air resistance for the moment...

In an inverted pendulum, the unbalancing torque increases as the tilt angle increases. In a rocket with rear-mounted motors, the unbalancing torque does not increase. As the rocket tilts, the motors tilt along with it. Their relative angle remains fixed and the unbalanced torque remains unchanged. The result is a fixed angular acceleration for the rocket.

In a normal pendulum, the restoring torque increases as the tilt angle increases. In a rocket with front-mounted motors, the restoring torque does not increase. As the rocket tilts, the motors tilt along with it. Their relative angle remains fixed and the unbalanced torque remains unchanged. The result is a fixed angular acceleration for the rocket.
 
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