Your videos are detailed and make a complicated topic so much easier. Keep up the great work. 👍
@utkarshgupta29724 жыл бұрын
Wonderful video bro. I have been struggling from a long time to build it . So thanku man ❤ . I am also building small scale thrust vector control rockets. It's very helpful 😇.
@praroopchanda94774 жыл бұрын
thanks man , u are really of great help for simulations ,i want to learn and you give very realistic examples...
@user-jr5wh8ed8s2 жыл бұрын
So useful. Extremely helpful video for beginners. Thanks.
@DaeroLee_Solid_Aerospace4 ай бұрын
Thank you for your useful video.
@lukealsmith5 жыл бұрын
Thanks for the shout out! Great video :)
@jlhw4923 жыл бұрын
This is a very nice tutorial. Thank you so much!
@emanuelcastanho4704 жыл бұрын
Why do you have different constant values? In the paper the mass is 5830 slug, on your code is 38901 slug.
@Crusader_No_Regret Жыл бұрын
Is it possible to obtain the complete trajectory of the rocket in the three axes (x,y,z) through this model of the article that takes into account only the pitch angle and the angle of attack?
@ilyasbendjeffal97582 жыл бұрын
I looove youu man ❤️❤️❤️
@JuhoSprite3 жыл бұрын
Here from terminal montage
@sreehari78284 жыл бұрын
Hai. While I running the code it show error Show" not enough input arguments" Pleas help me.
@clefmonnaadipuo60165 жыл бұрын
Nice videos
@marcoasbernardes5 жыл бұрын
Excelent!
@linhanqiao34034 жыл бұрын
MASB 老哥少了个l
@user-yb2hq3km7h3 жыл бұрын
Very nice video!! Great job! There is just this thing I don't understand (I am trying to build a state space model of my team's rocket in order to use it to design airbrakes for the rocket), I checked the paper you mentioned, what parameters should I take under consideration? How to I adjust this state space matrices to my rocket?
@omerfarslan_2 жыл бұрын
Hi, I wonder can we use LQR method for real applications since the measuring the desired states is not so simple in real life. If the measurement is wrong, I assume control system may pushes the system to divergence. What about classical control approaches, that are more reliable and easy to handle?
@siddhantpanigrahi97003 жыл бұрын
Hi there , thanks for the informative videos, I have built a 6 dof simulation in simulink but I am stuck in the control surface block ....Can you help me out please..... Thanks in advance !!
@prashantbharati18673 жыл бұрын
Hey i only have a 4 input state space block in my matlab version. Can you suggest an alternative approach, as in how should i mould it in use as a single input source
@hafizuddinmohdlowhim84263 жыл бұрын
you also have video on launch and land rocket. you use different equations. what is the difference?
@VDEngineering3 жыл бұрын
One is linear other is not
@lac199513 жыл бұрын
Can you suggest a book that talks about modelling for Aerospace vehicles.
@vincentkivuva5844 жыл бұрын
Thanks for this. Am getting this error once I connect the gain output to the sate-space system: Data type mismatch. Output port 1 of 'LQR_Control/Gain' is a signal of data type 'boolean'. However, it is driving a signal of data type 'double'.
@anupamam5537 Жыл бұрын
Sir can you make a video about control allocation of reaction control syatem in RLV i really need help
@VDEngineering Жыл бұрын
possibly
@anupamam5537 Жыл бұрын
@@VDEngineering sir can you make a video regarding the milp control allocation part of the paper 'Quantized control allocation of reaction control jets and aerodynamic control surfaces' can you please help me sir 🙏
@alessandrovitiello38004 жыл бұрын
Hello, great video, many compliments could you explain better the MatLab part : for i = 1:100000 e_val(:,i) = eig(A_m - B_m*K*i/10000); end why you use the number 1e5 e 1e4, why you do *i/10000 yes, I know that the aim is to study the stability but I would like to understand better why your code has this approach in MatLab. and for k = 1:1 ....... why we use also this for a cycle, we do not do a cycle because is for one to one many thanks for your time and consideration