How Missile System Works | ATACMS MLRS

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This is ATACMS missile and is basically a Solid Fuel rocket propulsion system.

The Missiles ascend post-launch using GPS for course adjustment; their fins move per visuals, directed by inertial navigation or military-grade GPS to hit designated targets; upon impact, the sensor triggers a 500-pound TNT blast, capable of bunker destruction.

Interestingly they can be operated from both platforms the HIMARS or the track version MLRS.

This requires a platform to transport with this Galaxy C-5 aircraft.
We will also look at the step-by-step process of how this works
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now thats some amazing animation and explanations. THX so much for the video, youre the best

Polish_Gopnik
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im here 5 months later after ATACMS made s400 a lawn ornament. 🤣

raz
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The missile knows where it is at all times. It knows this because it knows where it isn't. By subtracting where it is from where it isn't, or where it isn't from where it is (whichever is greater), it obtains a difference, or deviation. The guidance subsystem uses deviations to generate corrective commands to drive the missile from a position where it is to a position where it isn't, and arriving at a position where it wasn't, it now is. Consequently, the position where it is, is now the position that it wasn't, and it follows that the position that it was, is now the position that it isn't.
In the event that the position that it is in is not the position that it wasn't, the system has acquired a variation, the variation being the difference between where the missile is, and where it wasn't. If variation is considered to be a significant factor, it too may be corrected by the GEA. However, the missile must also know where it was.
The missile guidance computer scenario works as follows. Because a variation has modified some of the information the missile has obtained, it is not sure just where it is. However, it is sure where it isn't, within reason, and it knows where it was. It now subtracts where it should be from where it wasn't, or vice-versa, and by differentiating this from the algebraic sum of where it shouldn't be, and where it was, it is able to obtain the deviation and its variation, which is called error.

MrVinicius
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" how fins work " keep up the good work !

MrPhantomFury
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It satisfactory to see the fact the missile has to be pointy

sagarjadhav
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The ATACMS uses laser based inertial guide systems (not the old mechanical gyroscope type). They are much more advanced and accurate.

KingLutherQ
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I am from India and like your video each time 🎉🎉🎉🎉🎉🎉

Sharma-hdgm
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3:30 can you really compare the ATACMS which is essentially a short range ballistic missile to cruise missiles?

Just_A_Random_Desk
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Thank you very much for that good explained and visualized video <3

NaNoXiDo
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You got the animation wrong. ATACMS is a tactical ballistic missile. It does not swerve and adjust like cruise missiles

TrusePkay
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Nice video and nice channel.
How the control fins are moving, there should be a servo or motor to move them . as well as a source of energy (Battery) to drive those motors.

Auday
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Question?
Regarding the Impact sensor at the beginning, is it possible that bad weather could interfere with its projected path or destination?
-Say Rain, Snow, Hail Fog, High Winds?

marshalllapenta
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Very informative speech enjoy it thank you .Geo prespective

williambrown
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Decent video. Some inaccuracies, but overall pretty solid.

NotMyRealEffingName
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Comparing the British & Russian cruise missile varriants to the ATACMS is comparing apples to oranges my man.

ronniebauman
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Can someone give more details about the rocket engine(motor)???

dragosbeian
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First up, love it. Keep up the good work.
But....
It is misleading to compare the speed of a rocket motor to the air breathing cruise missiles that you used as an example.
That's all.

traviscaines
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@ 3:51, it is not appropriate at all to compare ballistic to cruise missiles in terms of speed.

nahidhkurdi
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4:34 “MLRS” is the type of vehicle, this one is called M270

eohq
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Are you comparing cruise missile to a ballistic one??

boulabiar